Peter Ott


Office: ME A2 434
EPFLSTISTI-SGMSGM-ENS

Expertise

Recherche expérimentale et numérique des écoulements stationnaires et instationnaires dans les turbomachines thermiques (inclut phénomènes de transfert de chaleur)

Publications représentatives

Combined 3-D flow and heat transfer measurements in a 2-pass internal coolant passage of gas turbine airfoils.

Chanteloup, D., Y. Juaneda, et al.
Published in Journal of Turbomachinery-Transactions of the Asme 124(4): 710-718., 2002 in

Flow characteristics in two-leg internal coolant passages of gas turbine airfoils with film-cooling hole ejection.

Chanteloup, D. and A. Bolcs
Published in Journal of Turbomachinery-Transactions of the Asme 124(3): 499-507., 2002 in

Particle image velocimetry investigation of the flow characteristics in two-leg internal coolant passages of gas turbine airfoils.

Chateloup, D. and A. Bolcs
Published in Proceedings of the Institution of Mechanical Engineers Part a- Journal of Power and Energy 215(A6): 743-752., 2001 in

Evidence for the Higgs Boson Decay to a Z Boson and a Photon at the LHC

G. AadB. AbbottK. AbelingN. J. AbichtS. H. Abidi  et al.

Physical Review Letters. 2024-01-11. DOI : 10.1103/PhysRevLett.132.021803.

Combination of inclusive top-quark pair production cross-section measurements using ATLAS and CMS data at √s=7 and 8 TeV

G. AadB. AbbottD. C. AbbottA. Abed AbudK. Abeling  et al.

Journal Of High Energy Physics. 2023-07-27. DOI : 10.1007/JHEP07(2023)213.

Celebration of Professor Bernhard Weigand on his 60th birthday

X. ChuG. YangA. TerzisV. VaikuntanathanW. Wang  et al.

International Journal Of Heat And Mass Transfer. 2022-06-01. DOI : 10.1016/j.ijheatmasstransfer.2022.122626.

Experimental investigation and analysis of sequential jet impingement concepts for enhanced turbine cooling

M. Gaffuri / J. A. SchiffmannP. Ott (Dir.)

Lausanne, EPFL, 2021. DOI : 10.5075/epfl-thesis-8721.

Transient Liquid Crystal Thermography Using a Time Varying Surface Heat Flux

J. SchmidM. GaffuriA. TerzisP. OttJ. von Wolfersdorf

International Journal of Heat and Mass Transfer. 2021-07-28. DOI : 10.1016/j.ijheatmasstransfer.2021.121718.

Heat Transfer Enhancement in a Double Sequential Impingement Channel

M. GaffuriP. OttS. NaikM. Henze

2021. ASME Turbo Expo 2021, virtual, online, June 7-11, 2021. DOI : 10.1115/GT2021-58913.

Experimental investigation of sequential narrow impingement channels for turbine cooling

M. GaffuriP. OttS. NaikM. Henze

2021. 14th European Confernce on Turbomachinery Fluid Dynamics & Thermodynamics, Gdansk, Pologne, April 12-16, 2021.

Mechanisms of Control Authority by Nanosecond Pulsed Dielectric Barrier Discharge Actuators on Flow Separation

C. SkouridesD. NyfantisP. LeylandH. BosseP. Ott

Applied Sciences. 2019. DOI : 10.3390/app9152989.

Narrow Impingement Channels: Recent Advancements and Future Directions

M. GaffuriA. TerzisP. Ott

2019. ETC13 - European Turbomachinery Conference, Lausanne, CH, April 8-12, 2019. DOI : 10.29008/ETC2019-252.

Measurement of the single top quark and antiquark production cross sections in the $t$ channel and their ratio in proton-proton collisions at $\sqrt{s}=$ 13 TeV

A. M. SirunyanA. TumasyanW. AdamF. AmbrogiE. Asilar  et al.

2018-12-26

Evaluation of Heat Transfer Coefficients for an Impingement Cooling Cascade: Experimental Challenges and Preliminary Results

M. GaffuriA. TerzisP. OttS. RetzkoM. Henze

2018. XXIV Biannual Symposium on Measuring Techniques in Turbomachinery, Prague, CZE, August 29-31, 2018.

Ammonia toxicity: from head to toe?

S. DasarathyR. P. MookerjeeV. RackayovaV. R. ThraneB. Vairappan  et al.

Metabolic Brain Disease. 2017. DOI : 10.1007/s11011-016-9938-3.

OES Characterization of Steamers in a Nanosecond Pulsed SBDB Using N2 and Ar Transitions

S. GoekceP. PeschkeC. HollensteinP. LeylandP. Ott

Plasma Soucre Science and Technology. 2016. DOI : 10.1088/0963-0252/25/4/045002.

Aerothermal Investigation of a Single Row Divergent Narrow Impingement Channel by Particle Image Velocimetry and Liquid Crystal Thermography

A. TerzisC. SkouridesP. OttJ. von WolfersdorfB. Weigand

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2016. DOI : 10.1115/1.4032328.

Investigation of Nanosecond Pulse Dielectric Barrier Discharges in Still Air and in Transonic Flow by Optical Methods

P. PeschkeS. GoekceP. LeylandP. Ott

IOP Journal of Physics D: Applied Physics. 2016. DOI : 10.1088/0022-3727/49/2/025204.

Improved Accuracy in Jet Impingement Heat Transfer Experiments Considering the Layer Thicknesses of a Triple Thermochromic Liquid Crystal Coating

A. TerzisS. BontitsopoulosP. OttJ. von WolfersdorfA. Kalfas

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2016. DOI : 10.1115/1.4031786.

On the Effects of Coating Thickness in Transient Heat Transfer Experiments Using Thermochromic Liquid Crystals

S. SchulzS. BrackA. TerzisJ. von WolfersdorfP. Ott

Experimental Thermal and Fluid Science. 2016. DOI : 10.1016/j.expthermflusci.2015.08.011.

High-Resolution Heat Transfer Measurements and Crossflow Regulation in Narrow Impingement Cooling Channels with Divergent Geometries

S. BontitsopoulosA. TerzisP. OttA. Kalfas

2015. 11th International Gas Turbine Congress, Tokyo, JP, November 15-20, 2015.

Impact of ns-DBD Plasma Actuation on the Boundary Layer Transition Using Convective Heat Transfer Measurements

D. UllmerP. PeschkeA. TerzisP. OttB. Weigand

IOP Journal of Physics D: Applied Physics. 2015. DOI : 10.1088/0022-3727/48/36/365203.

Investigation of Flow Separation Control by Nanosecond Pulsed Dielectric Barrier Discharge Actuators

N. GrechP. LeylandP. PeschkeP. Ott

Progress in Flight Physics; Moscow: EUCASS, Torus Press, 2015. p. 191-210.

Heat Transfer Characteristics of High Crossflow Impingement Channels: Effect of Number of Holes

S. LluciàA. TerzisP. OttM. Cochet

Proceedings of IMechE, Part A: Journal of Power and Energy. 2015. DOI : 10.1177/0957650915594074.

Aeroeleasic Investigation of an Annular Transonic Compressor Cascade: Experimental Results

V. A. ChenauxA. ZankerP. Ott

2015. ASME Turbo Expo 2015, Montreal, CA, June 15-19, 2015. DOI : 10.1115/GT2015-43317.

Turbulent scale resolving modelling of rotating stall in low-pressure steam turbines operated under low volume flow conditions

B. MegerleT. S. RiceI. McBeanP. Ott

2015. ASME Turbo Expo 2015, Montreal, CA, June 15-19, 2015. DOI : 10.1115/GT2015-42498.

On the Applicability of a Triple Thermochromic Liquid Crystal Layer for Transient Heat Transfer Experiments

S. BontitsopoulosA. TerzisP. OttA. Kalfas

2015. 1st Thermal and Fluids Engineering Summer Conference (TFESC-1), New York City, USA, August 9-12, 2015.

Heat Transfer Characteristics of High Crossflow Impingement Channels: Effect of Number of Holes

S. LluciàA. TerzisP. OttM. Cochet

2015. 11th European Turbomachinery Conference, Madrid, SP, March 23-27, 2015. p. 1-10.

A method to visualise near wall fluid flow patterns using locally resolved convective heat transfer experiments

A. TerzisJ. von WolfersdorfB. WeigandP. Ott

Experimental Thermal and Fluid Science. 2015. DOI : 10.1016/j.expthermflusci.2014.09.009.

Effect of Varying Jet Diameter on the Heat Transfer Distributions of Narrow Impingement Channels

A. TerzisP. OttM. CochetJ. von WolfersdorfB. Weigand

Journal of Turbomachinery. 2015. DOI : 10.1115/1.4028294.

Fluid Flow Pattern Visualisation: An Alternative Approach Using Highly Resolved Heat Transfer Experiments

A. TerzisP. OttJ. von WolfersdorfB. Weigand

2014. XXII Symposium on Measuring Techniques in Turbomachinery, Lyon, F, September 4-5, 2014.

EPFL-GTT: Group of Thermal Turbomachinery

P. Ott

ERCOFTAC Bulletin. 2014.

Plasma Diagnostics and Modelling of Nanosecond Pulsed Surface Dielectric Barrier Discharge Actuators

S. Goekce / P. Ott (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6282.

Experimental Investigation of Pulsed DBD Plasma Actuators for Aerodynamic Flow Control

P. Peschke / P. Ott (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6265.

Experimental Investigation of Blade Group Vibrations in an Axial Turbine Cascade

A. Zanker / P. Ott (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6194.

Detailed Heat Transfer Distributions of Narrow Impingement Channels with Varying Jet Diameter

A. TerzisM. CochetJ. von WolfersdorfB. WeigandP. Ott

2014. GT-2014: ASME Turbo Expo 2014, Düsseldorf, D, June 16-20, 2014. p. 1-11. DOI : 10.1115/GT2014-25910.

Experimental and Numerical Assessment of the Aeroelastic Stability of Blade Pair Packages

A. VegaR. CorralA. ZankerP. Ott

2014. GT-2014: ASME Turbo Expo 2014, Düsseldorf, D, June 16-20, 2014. p. 1-12. DOI : 10.1115/GT2014-25607.

Detailed Heat Transfer Distributions of Narrow Impingement Channels for Cast-In Turbine Airfoils

A. TerzisP. OttJ. von WolfersdorfB. WeigandM. Cochet

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2014. DOI : 10.1115/1.4027679.

Detailed heat transfer distributions of narrow impingement channels for integrally cast turbine airfoils

A. Terzis / P. Ott (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6177.

Unsteady aerodynamics of low-pressure steam turbines operating under low volume flow conditions

B. Megerle / P. OttI. W. McBean (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6096.

Unsteady Aerodynamics of Low-Pressure Steam Turbines Operating Under Low Volume Flow

B. MegerleI. McBeanT. S. RiceP. Ott

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2014. DOI : 10.1115/1.4027373.

Hole Staggering Effect on the Cooling Performance of Narrow Impingement Channels Using the Transient Liquid Crystal Technique

A. TerzisG. WagnerJ. von WolfersdorfP. OttB. Weigand

Transactions- American Society of Mechanical Engineers Journal of Heat Transfer. 2014. DOI : 10.1115/1.4027250.

A Comparative Study of the Local Heat Transfer Distributions Around Various Surface Mounted Obstacles

R. WyssmannD. UllmerA. TerzisP. Ott

Journal of Thermal Science. 2014. DOI : 10.1007/s11630-014-0692-8.

Numerical and Experimental Investigations of an Annular Transonic Compressor Cascade Considering Leakage Flows

V. A. ChenauxM. BlocherP. Ott

2014. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-15), Honolulu, USA, February 24-28, 2014.

Local Heat Transfer Distributions of Small Impingement Configurations: A Detailed Experimental Procedure Using Transient Heat Transfer Methods

A. TerzisJ. von WolfersdorfB. WeigandP. Ott

2014. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-15), Honolulu, USA, February 24 - 28, 2014.

Experimental and numerical investigation of narrow impingement cooling channels

S. FechterA. TerzisP. OttB. WeigandJ. Von Wolfersdorf  et al.

International Journal Of Heat And Mass Transfer. 2013. DOI : 10.1016/j.ijheatmasstransfer.2013.09.003.

Experimental Aeroelastic Investigation of Vibrating Turbine Blade Clusters

A. ZankerP. OttP. Calza

18th Blade Mechanics Seminar, Winterthur, CH, September 11, 2013.

Unsteady Aerodynamics of Low-Pressure Steam Turbines Operating Under Low Volume Flow

B. MegerleT. S. RiceI. McBeanP. Ott

ANSYS Conference & 18th Swiss CADFEM Users‘ Meeting, Zurich, CH, September 05-06, 2013.

Experimental and Numerical Investigation of a Fully Confined Impingement Round Jet

O. CaggeseG. GnaegiG. HannemaA. TerzisP. Ott

International Journal of Heat and Mass Transfer. 2013. DOI : 10.1016/j.ijheatmasstransfer.2013.06.043.

Investigation of Flow Separation Control by Nanosecond Pulsed Dielectric Barrier Discharge Actuators

N. GrechP. PeschkeS. BustamenteP. LeylandP. Ott

2013. EUCCAS 2013 – 5th European Conference for Aeronautics and Space Sciences, Munich, Germany, July 1-5, 2013.

Experimental Investigation of Pulsed Dielectric Barrier Discharge Actuators in Sub- and Transonic Flow

P. PeschkeS. GoekceP. LeylandC. HollensteinP. Ott

2013. 44th AIAA Plasmadynamics and Lasers Conference, San Diego, CA, USA, June 24-27, 2013. DOI : 10.2514/6.2013-2885.

Experimental Aeroelastic Analysis of Clustered Turbine Blades Vibrating in Mixed Torsion/Bending Mode

A. ZankerP. OttP. Calza

2013. 31st AIAA Applied Aerodynamics Conference, San Diego, CA, USA, June 24-27, 2013. DOI : 10.2514/6.2013-3152.

Unsteady Aerodynamics of Low-Pressure Steam Turbines Operating Under Low Volume Flow

B. MegerleT. S. RiceI. McBeanP. Ott

2013. ASME Turbo Expo 2013, San Antonio, Texas, USA, June 3-7, 2013. DOI : 10.1115/GT2013-95409.

Evolution of the Aerodynamic Stability of an Oscillating Annular Compressor Cascade with Inlet Reverse Flow Condition Variations

V. ChenauxH. SchönenbornP. Ott

2013. ETC10 - 10th European Conference on Turbomachinery, Lappeenranta, FI, April 14-19, 2013. p. 907-916.

Experimental Aeroelastic Investigation of Vibrating Turbine Blade Clusters

A. ZankerP. OttP. Calza

2013. ETC10 - 10th European Conference on Turbomachinery, Lappeenranta, FI, April 14-19, 2013. p. 210-221.

High Voltage Pulsed DBD Effects on the Aerodynamic Performances and on the Shock Buffet

A. MarinoP. PeschkeF. De GregorioP. LeylandP. Ott  et al.

ERCOFTAC Bulletin. 2013.

Numerical and Experimental Investigation of the Aerodynamic Excitation of a Model Low-Pressure Steam Turbine Stage Operating Under Low Volume Flow

B. MegerleT. S. RiceI. W. McBeanP. Ott

Journal of Engineering for Gas Turbines and Power. 2013. DOI : 10.1115/1.4007334.

High Voltage Pulsed DBD Effects on the Aerodynamic Performances and on the Shock Buffet

A. MarinoP. PeschkeF. De GregorioP. LeylandP. Ott  et al.

Joint ERCOFTAC/PLASMAERO Public Workshop, Toulouse; F, December 10-12, 2012.

Thermocouple Thermal Inertia Effects on Impingement Heat Transfer Experiments Using the Transient Liquid Crystal Technique

A. TerzisJ. von WolfersdorfB. WeigandP. Ott

Measurement Science and Technology. 2012. DOI : 10.1088/0957-0233/23/11/115303.

Characterization of Kinetic Processes in Nano Pulsed SDBD

S. GoekceP. PeschkeC. HollensteinP. LeylandP. Ott

2012. NEPCAP 2012 - 5th International Symposium on "Non-Equilibrium Processes, Plasma, Combustion, and Atmospheric Phenomena", Sochi (Loo), RU, October 1-6, 2012.

Experimental Investigations of an Oscillating Annular Compressor Cascade at Reverse Flow Conditions

V. A. ChenauxH. SchönenbornP. Ott

2012. ISUAAAT13 - 13th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, Tokyo, JP, September 11-14, 2012.

Aerodynamic Excitation of a Model Low-Pressure Steam Turbine Stage Under Low Volume Flow

B. MegerleT. S. RiceI. W. McBeanP. Ott

17th Blade Mechanics Seminar, Winterthur, CH, September 12, 2012.

Investigation of High-Pressure Turbine Endwall Film-Cooling Performance Under Realistic Inlet Conditions

S. SalvadoriL. OttanelliM. JonssonP. OttF. Martelli

AIAA Journal of Propulsion and Power. 2012. DOI : 10.2514/1.59225.

Hole Staggering Effect on the Cooling Performance of Narrow Impingement Channels

A. TerzisG. WagnerP. Ott

2012. ASME Turbo Expo 2012 (GT2012), Copenhagen, DK, June 11-15, 2012. p. 127-138. DOI : 10.1115/GT2012-68323.

Numerical and Experimental Investigation of the Aerodynamic Excitation of a Model Low-Pressure Steam Turbine Stage Operating Under Low Volume Flow

B. MegerleT. S. RiceI. W. McBeanP. Ott

2012. ASME Turbo Expo 2012 (GT2012), Copenhagen, DK, June 11-15, 2012. p. 403-414. DOI : 10.1115/GT2012-68384.

Swirl Jets in Crossflow at Low Velocity Ratios

A. TerzisC. KazakosA. KalfasP. ZachosP. Ott

Journal of Mechanics Engineering and Automation. 2012.

Experimental Investigation of the Aeroelastic Stability of an Annular Compressor Cascade at Reverse Flow Conditions

V. A. Chenaux / P. Ott (Dir.)

Lausanne, EPFL, 2012. DOI : 10.5075/epfl-thesis-5358.

Heat Transfer and Performance Characteristics of Axial Cooling Fans with Downstream Guide Vanes

A. TerzisI. StylianouA. KalfasP. Ott

Journal of Thermal Science. 2012. DOI : 10.1007/s11630-012-0531-8.

Influence of Thermocouple Thermal Inertia in Impingement Heat Transfer Experiments Using Transient Techniques

A. TerzisJ. von WolfersdorfG. WagnerB. WeigandP. Ott

2012. XXI Biannual Symposium on Measuring Techniques in Turbomachinery, Valencia, E, March 22-23, 2012.

Investigation of High Pressure Turbine End-Wall Film Cooling Performances under Realistic Inlet Conditions

S. SalvadoriL. OttanelliM. JonssonF. MartelliP. Ott

2011. XX International Symposium on Air Breathing Engines (ISABE), Gothenburg, S, September 12-16, 2011.

Investigation on the Three-Dimensional Flow Mechanisms in Annular Axial Compressor Cascades for Aero Engines with Flow Control by Aspiration on the Hub and on the Blades

E. Colombo / P. Ott (Dir.)

Lausanne, EPFL, 2011. DOI : 10.5075/epfl-thesis-5241.

Effect of Stators on the Performance and the Thermal Capabilities of Small Axial Cooling Fans

A. TerzisI. StylianouA. KalfasP. Ott

2011. 10th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows (ISAIF-10), Brussels, Belgium, 4-7 July, 2011.

Interaction Between Nanosecond Pulse DBD Actuators and Transonic Flow

P. PeschkeS. GoekceC. HollensteinP. LeylandP. Ott

2011. 41st AIAA Fluid Dynamics Conference and Exhibit, Honolulu, HI, USA, June 27-40, 2011. DOI : 10.2514/6.2011-3734.

Aeroelasticity at Reversed Flow Conditions – Part 1: Numerical and Experimental Investigations of a Compressor Cascade with Controlled Vibration

H. SchönenbornV. ChenauxP. Ott

2011. ASME Turbo Expo 2011, Power for Land, Sea & Air, Vancouver, CAN, June 6-10, 2011. p. 1171-1181. DOI : 10.1115/GT2011-45034.

Electron temperature measurements using N2 and Argon transitions in an ATP fast pulsed DBD

S. GoekceP. PeschkeP. OttC. HollensteinP. Leyland

2011 Aerospace Thematic Workshop at Les Houches (Fundamentals of Aerodynamic Flow and Combustion Control by Plasmas), Les Houches, France, March 27 - April 01, 2011.

Experimental Investigations of the Aerodynamics of an Annular Compressor Cascade at Reversed Flow Conditions

V. ChenauxH. SchönenbornP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 249-259.

Swirl Jet and Crossflow Interaction at Low Velocity Ratios and Incompressible Flows

A. TerzisC. KazakosP. ZachosA. KalfasP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 133-144.

Influence of Blade Aspiration on the Flow Quality of an Annular Axial Compressor Cascade

E. ColomboL. CastillonP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 1345-1356.

Characterization of the Flow Generated in an Annular Test Facility

C. DeslotE. ColomboF. LeboeufD. CharbonnierP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 1413-1424.

Investigation of End-Wall Film Cooling Configuration Performances in a Linear Cascade

S. SalvadoriL. OttanelliF. MartelliM. JonssonP. Ott

2010. 65° Congresso Nazionale ATI, Cagliari, Italy, September 13-17, 2010.

Aero Engine Flow Control by Surface Discharge Plasma

S. GoekceP. PeschkeC. HollensteinP. OttP. Leyland

2010. III International Scientific and Technical Conference - Aeroengines of XXI Century, Moscow, RU, November 30 - December 3, 2010.

Heat Transfer Measurements in a Turbine Cascade: Taking Advantage of the Thermal Bahaviour of a PSP Sensor

M. JonssonP. Ott

2010. XX Biannual Symposium on Measuring Techniques in Turbomachinery, Transonic and Supersonic Flow in Cascades and Turbomachines, Milano, Italy, September 23-24, 2010.

Surface DBD’s and plasma-flow interaction

S. GoekceP. PeschkeC. HollensteinP. LeylandP. Ott  et al.

2010. Euromech Fluid Mechanics Conference - 8, Bad Reichenhall, D, September 13-16, 2010.

Investigations on Axial Compressor Cascades with Aspiration on Blades and Hub

E. ColomboC. DeslotP. OttF. BarioL. Castillon  et al.

European Workshop on New Aero Engine Concepts, Munich, Germany, June 30-July 1, 2010.

Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling

M. Jonsson / P. Ott (Dir.)

Lausanne, EPFL, 2010. DOI : 10.5075/epfl-thesis-4650.

EPFL-LTT: Turbomachinery Laboratory

P. Ott

ERCOFTAC Bulletin. 2009.

Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform

D. CharbonnierP. OttM. JonssonF. CottierT. Köbke

2009. ASME Turbo Expo 2009, Orlando, Fl, USA, June 8-12, 2009. p. 1027-1038. DOI : 10.1115/GT2009-60306.

Effects of a surface dielectric barrier discharge on transonic flows around an airfoil

S. PavonP. OttP. LeylandJ.-L. DorierC. Hollenstein

2009. 47th AIAA Aerospace Sciences Meeting, Orlando, Florida, USA, January 05-08, 2009. DOI : 10.2514/6.2009-649.

Interaction between a surface dielectric barrier discharge and transonic airflows

S. Pavón / P. OttJ. R. Thome (Dir.)

Lausanne, EPFL, 2008. DOI : 10.5075/epfl-thesis-4201.

Comparison of Numerical Investigations With Measured Heat Transfer Performance of a Film Cooled Turbine Vane

D. CharbonnierP. OttM. JonssonT. KöbkeF. Cottier

2008. 53rd ASME Turbo Expo 2008, Berlin, Germany, June 9-13, 2008. p. 571-582. DOI : 10.1115/GT2008-50623.

Application of the Transient Heater Foil Technique for Heat Transfer and Film Cooling Effectiveness Measurements on a Turbine Vane Endwall

M. JonssonD. CharbonnierP. OttJ. von Wolfersdorf

2008. 53rd ASME Turbo Expo 2008, Berlin, Germany, June 9-13, 2008. p. 443-453. DOI : 10.1115/GT2008-50451.

Application of the Transient Heater Foil Technique for Heat Transfer Measurements

M. JonssonP. Ott

2008. XIX Biannual Symposium on Measuring Techniques in Turbomachinery, VKI, Rhode-St-Genèse, Belgium, April 7-8, 2008.

Numerical Analysis of Adiabatic Film Cooling Effectiveness Around HP-Turbine Airfoil – Decomposed Computation of Internal-External Airflows

D. CharbonnierM. JonssonP. Ott

2008. ISROMAC-12, Honolulu, Hawaii, USA, 17-22 February, 2008.

LONG LIFETIME SYSTEM FOR THE GENERATION OF SURFACE PLASMAS

S. PAVONA. SUBLETJ. DORIERC. HOLLENSTEINP. LEYLAND  et al.

WO2009098662 . 2007.

Leading Edge Film Cooling and the Influence of Fan Shaped Holes at Design and Off-Design Conditions

G. WagnerP. OttG. VogelS. Naik

2007. ASME Turbo Expo 2007, Montreal, Canada, May 14-17, 2007. p. 577-587. DOI : 10.1115/GT2007-27715.

Effects of high-speed airflows on a surface dielectric barrier discharge

S. Pavon-L. DorierC. HollensteinP. OttP. Leyland

Journal of Physics D : Applied Physics. 2007. DOI : 10.1088/0022-3727/40/6/021.

Heat Transfer Experiments on an Heavily Film Cooled Nozzle Guide Vane

M. JonssonP. Ott

2007. 7th European Turbomachinery Conference - ETC7, Athens, Greece, 5-9 March 2007. p. 1011-1020.

Analysis of the Cooling Performance on a Showerhead Cooled Blunt Body using the Wall Cooling Effectiveness

E. ColomboG. WagnerJ. von WolfersdorfP. Ott

2007. 7th European Turbomachinery Conference - ETC7, Athens, Greece, 5-9 March 2007. p. 989-998.

Experimental Investigation of Combined/Simultaneous Gust and Oscillating Turbine Row Unsteady Aerodynamics in Transonic Flow

A. BerettaF. RottmeierP. Ott

2007. 7th European Turbomachinery Conference - ETC7, Athens, Greece, 5-9 March 2007. p. 1285-1297.

Effect of transonic airflows on a dielectric barrier discharge

S. PavonJ.-L. DorierC. HollensteinP. OttP. Leyland

2006. Gordon Research Conference on Processing Plasmas, Mount Holyoke College, South Hadley, MA, USA, July 16-21, 2006.

Temperature and Pressure Sensitive Coatings

J. von WolfersdorfP. OttB. Weigand

Flow Phenomena in Nature, Volume 2 - Inspiration, Learning and Application; Southampton, UK: WIT Press, 2006. p. 747-766.

Experimental Investigations of Turbine Blade Showerhead Cooling

G. WagnerG. VogelP. Ott

2006. 13th International Heat Transfer Conference (IHTC-13), Sydney, Australia, August 13 - 18, 2006.

Influence of Mainstream Incidence Angle on Leading Edge Film Cooling Measured by the Transient Liquid Crystal Technique

G. WagnerP. OttG. Vogel

2006. 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-11), Honolulu, Hawaii, February 26 - March 2, 2006.

Effects of transonic air flows on a dielectric barrier discharge

S. Pavon-L. DorierC. HollensteinP. OttP. Leyland

2006. Gordon Research Conference on Plasma Processing Science (GRC-PPS), Mount Holyoke College, South Hadley, MA, July 16-21, 2006.

Experimental investigations on showerhead cooling on a blunt body

C. FalcozB. WeigandP. Ott

International Journal of Heat and Mass Transfer. 2006. DOI : 10.1016/j.ijheatmasstransfer.2005.10.012.

A comparative study on showerhead cooling performance

C. FalcozB. WeigandP. Ott

International Journal of Heat and Mass Transfer. 2006. DOI : 10.1016/j.ijheatmasstransfer.2005.10.013.

Combined/simultaneous gust and oscillating turbine row unsteady aerodynamics in subsonic flow

A. BerettaF. RottmeierP. Ott

Experimental Thermal and Fluid Science. 2006. DOI : 10.1016/j.expthermflusci.2005.09.001.

Influence of Modeshape Mistuning on the Forced Response of a Turbine Cascade

A. BerettaG. KahlP. Ott

2006. 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-11), Honolulu, Hawaii, February 26 - March 2, 2006.

Method for Analysis of Showerhead Film Cooling Experiments on Highly Curved Surfaces

G. WagnerE. SchneiderJ. v. WolfersdorfP. OttB. Weigand

2005. 6th European Turbomachinery Conference - ETC6, Lille, France, 7-11 March 2005. p. 381-389. DOI : 10.1016/j.expthermflusci.2006.05.006.

The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

G. WagnerM. KotullaP. OttB. WeigandJ. von Wolfersdorf

Journal of Turbomachinery. 2005. DOI : 10.1115/1.1811089.

Combined/Simultaneous Gust and Oscillating Turbine Row Unsteady Aerodynamics in Subsonic Flow

A. BerettaF. RottmeierP. Ott

2005.

The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

G. WagnerM. KotullaP. OttB. WeigandJ. von Wolfersdorf

2004. p. 521-531. DOI : 10.1115/GT2004-53553.

Boundary Layer Suction via a Slot in a Transonic Compressor - Numerical Parameter Study and First Results

K. HubrichA. BölcsP. Ott

2004. p. 527-536. DOI : 10.1115/GT2004-53758.

Experimental Investigation of an Oscillating Airfoil in the Prescence of Downstream-Generated Aerodynamic Gusts

M. NowinskiP. OttA. Bölcs

2000.

Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi 3D Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

T. H. FranssonM. JöckerA. BölcsP. Ott

Journal of Turbomachinery. 1999. DOI : 10.1115/1.2836725.

The Influence of Tailboards on Unsteady Measurements in a Linear Cascade

P. OttM. NorrydA. Bölcs

1998. p. 98-GT-572. DOI : 10.1115/98-GT-572.

Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi 3D Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

T. H. FranssonM. JöckerA. BölcsP. Ott

1998. p. 98-GT-490. DOI : 10.1115/98-GT-490.

A Basic Forced Response Experiment

M. NowinskiP. Ott

1997. 8th International Symposium, Stockholm, Sweden, 14–18 September 1997. p. 665–678. DOI : 10.1007/978-94-011-5040-8_43.

Computation of Unsteady 3-D Transonic Nozzle Flows due to Fluctuating Back-Pressure using k-e Turbulence Closure

G. GerolymosI. ValletP. OttA. Bölcs

AIAA Journal. 1996. DOI : 10.2514/3.13237.

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

P. OttA. BölcsT. H. Fransson

Journal of Turbomachinery. 1995. DOI : 10.1115/1.2835625.

Computation of Unsteady 3-D Transonic Flows due to Fluctuating Back-Pressure using k-e Turbulence Closure

G. A. GerolymosI. ValletP. OttA. Bölcs

1995. IMACS-COST Conference Computational Fluid Dynamics Three-Dimensional Complex Flows, Lausanne, September 13- 15, 1995.

Turbine Calculations With Structured and Unstructured Meshes

P. LeylandP. OttR. Richter

1994.

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

P. OttA. BölcsT. H. Fransson

1993. p. 93-GT-139. DOI : 10.1115/93-GT-139.

Oszillierender senkrechter Verdichtungsstoss in einer ebenen Düse

P. Ott / A. Bölcs (Dir.)

Lausanne, EPFL, 1992. DOI : 10.5075/epfl-thesis-985.

Unsteady pressure response to an oscillating normal schock wave in a nozzle

P. OttA. BölcsT. H. Fransson

1992. 11th Symposium on Measuring Techniques in Transonic and Supersonic Flow in Cascades and Turbomachines, München, Germany, 14-15 September 1992.

Numerical Computation of Unsteady Inviscid Transonic Flow Through Nozzles With Fluctuating Back Pressure

A. BölcsT. FranssonP. Ott

EPFL Supercomputing Review. 1988.

Unsteady Flow Visualization in a Vibrating Annular Turbine Cascade Operating in the Transonic Flow Regime

A. BölcsF. JollesP. OttD. Schläfli

1987. 4th International Symposium on Unsteady Aerodynamics and Aeroelasticity in Turbomachines and Propellers, Aachen, Germany, September 6-10, 1987.

Celebration of Professor Bernhard Weigand on his 60th birthday

X. ChuG. YangA. TerzisV. VaikuntanathanW. Wang  et al.

International Journal Of Heat And Mass Transfer. 2022-06-01. DOI : 10.1016/j.ijheatmasstransfer.2022.122626.

Experimental investigation and analysis of sequential jet impingement concepts for enhanced turbine cooling

M. Gaffuri / J. A. SchiffmannP. Ott (Dir.)

Lausanne, EPFL, 2021. DOI : 10.5075/epfl-thesis-8721.

Transient Liquid Crystal Thermography Using a Time Varying Surface Heat Flux

J. SchmidM. GaffuriA. TerzisP. OttJ. von Wolfersdorf

International Journal of Heat and Mass Transfer. 2021-07-28. DOI : 10.1016/j.ijheatmasstransfer.2021.121718.

Heat Transfer Enhancement in a Double Sequential Impingement Channel

M. GaffuriP. OttS. NaikM. Henze

2021. ASME Turbo Expo 2021, virtual, online, June 7-11, 2021. DOI : 10.1115/GT2021-58913.

Experimental investigation of sequential narrow impingement channels for turbine cooling

M. GaffuriP. OttS. NaikM. Henze

2021. 14th European Confernce on Turbomachinery Fluid Dynamics & Thermodynamics, Gdansk, Pologne, April 12-16, 2021.

Mechanisms of Control Authority by Nanosecond Pulsed Dielectric Barrier Discharge Actuators on Flow Separation

C. SkouridesD. NyfantisP. LeylandH. BosseP. Ott

Applied Sciences. 2019. DOI : 10.3390/app9152989.

Narrow Impingement Channels: Recent Advancements and Future Directions

M. GaffuriA. TerzisP. Ott

2019. ETC13 - European Turbomachinery Conference, Lausanne, CH, April 8-12, 2019. DOI : 10.29008/ETC2019-252.

Evaluation of Heat Transfer Coefficients for an Impingement Cooling Cascade: Experimental Challenges and Preliminary Results

M. GaffuriA. TerzisP. OttS. RetzkoM. Henze

2018. XXIV Biannual Symposium on Measuring Techniques in Turbomachinery, Prague, CZE, August 29-31, 2018.

OES Characterization of Steamers in a Nanosecond Pulsed SBDB Using N2 and Ar Transitions

S. GoekceP. PeschkeC. HollensteinP. LeylandP. Ott

Plasma Soucre Science and Technology. 2016. DOI : 10.1088/0963-0252/25/4/045002.

Aerothermal Investigation of a Single Row Divergent Narrow Impingement Channel by Particle Image Velocimetry and Liquid Crystal Thermography

A. TerzisC. SkouridesP. OttJ. von WolfersdorfB. Weigand

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2016. DOI : 10.1115/1.4032328.

Investigation of Nanosecond Pulse Dielectric Barrier Discharges in Still Air and in Transonic Flow by Optical Methods

P. PeschkeS. GoekceP. LeylandP. Ott

IOP Journal of Physics D: Applied Physics. 2016. DOI : 10.1088/0022-3727/49/2/025204.

Improved Accuracy in Jet Impingement Heat Transfer Experiments Considering the Layer Thicknesses of a Triple Thermochromic Liquid Crystal Coating

A. TerzisS. BontitsopoulosP. OttJ. von WolfersdorfA. Kalfas

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2016. DOI : 10.1115/1.4031786.

On the Effects of Coating Thickness in Transient Heat Transfer Experiments Using Thermochromic Liquid Crystals

S. SchulzS. BrackA. TerzisJ. von WolfersdorfP. Ott

Experimental Thermal and Fluid Science. 2016. DOI : 10.1016/j.expthermflusci.2015.08.011.

High-Resolution Heat Transfer Measurements and Crossflow Regulation in Narrow Impingement Cooling Channels with Divergent Geometries

S. BontitsopoulosA. TerzisP. OttA. Kalfas

2015. 11th International Gas Turbine Congress, Tokyo, JP, November 15-20, 2015.

Impact of ns-DBD Plasma Actuation on the Boundary Layer Transition Using Convective Heat Transfer Measurements

D. UllmerP. PeschkeA. TerzisP. OttB. Weigand

IOP Journal of Physics D: Applied Physics. 2015. DOI : 10.1088/0022-3727/48/36/365203.

Investigation of Flow Separation Control by Nanosecond Pulsed Dielectric Barrier Discharge Actuators

N. GrechP. LeylandP. PeschkeP. Ott

Progress in Flight Physics; Moscow: EUCASS, Torus Press, 2015. p. 191-210.

Heat Transfer Characteristics of High Crossflow Impingement Channels: Effect of Number of Holes

S. LluciàA. TerzisP. OttM. Cochet

Proceedings of IMechE, Part A: Journal of Power and Energy. 2015. DOI : 10.1177/0957650915594074.

Aeroeleasic Investigation of an Annular Transonic Compressor Cascade: Experimental Results

V. A. ChenauxA. ZankerP. Ott

2015. ASME Turbo Expo 2015, Montreal, CA, June 15-19, 2015. DOI : 10.1115/GT2015-43317.

Turbulent scale resolving modelling of rotating stall in low-pressure steam turbines operated under low volume flow conditions

B. MegerleT. S. RiceI. McBeanP. Ott

2015. ASME Turbo Expo 2015, Montreal, CA, June 15-19, 2015. DOI : 10.1115/GT2015-42498.

On the Applicability of a Triple Thermochromic Liquid Crystal Layer for Transient Heat Transfer Experiments

S. BontitsopoulosA. TerzisP. OttA. Kalfas

2015. 1st Thermal and Fluids Engineering Summer Conference (TFESC-1), New York City, USA, August 9-12, 2015.

Heat Transfer Characteristics of High Crossflow Impingement Channels: Effect of Number of Holes

S. LluciàA. TerzisP. OttM. Cochet

2015. 11th European Turbomachinery Conference, Madrid, SP, March 23-27, 2015. p. 1-10.

A method to visualise near wall fluid flow patterns using locally resolved convective heat transfer experiments

A. TerzisJ. von WolfersdorfB. WeigandP. Ott

Experimental Thermal and Fluid Science. 2015. DOI : 10.1016/j.expthermflusci.2014.09.009.

Effect of Varying Jet Diameter on the Heat Transfer Distributions of Narrow Impingement Channels

A. TerzisP. OttM. CochetJ. von WolfersdorfB. Weigand

Journal of Turbomachinery. 2015. DOI : 10.1115/1.4028294.

Fluid Flow Pattern Visualisation: An Alternative Approach Using Highly Resolved Heat Transfer Experiments

A. TerzisP. OttJ. von WolfersdorfB. Weigand

2014. XXII Symposium on Measuring Techniques in Turbomachinery, Lyon, F, September 4-5, 2014.

EPFL-GTT: Group of Thermal Turbomachinery

P. Ott

ERCOFTAC Bulletin. 2014.

Experimental Investigation of Blade Group Vibrations in an Axial Turbine Cascade

A. Zanker / P. Ott (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6194.

Detailed Heat Transfer Distributions of Narrow Impingement Channels with Varying Jet Diameter

A. TerzisM. CochetJ. von WolfersdorfB. WeigandP. Ott

2014. GT-2014: ASME Turbo Expo 2014, Düsseldorf, D, June 16-20, 2014. p. 1-11. DOI : 10.1115/GT2014-25910.

Experimental and Numerical Assessment of the Aeroelastic Stability of Blade Pair Packages

A. VegaR. CorralA. ZankerP. Ott

2014. GT-2014: ASME Turbo Expo 2014, Düsseldorf, D, June 16-20, 2014. p. 1-12. DOI : 10.1115/GT2014-25607.

Detailed Heat Transfer Distributions of Narrow Impingement Channels for Cast-In Turbine Airfoils

A. TerzisP. OttJ. von WolfersdorfB. WeigandM. Cochet

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2014. DOI : 10.1115/1.4027679.

Detailed heat transfer distributions of narrow impingement channels for integrally cast turbine airfoils

A. Terzis / P. Ott (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6177.

Unsteady aerodynamics of low-pressure steam turbines operating under low volume flow conditions

B. Megerle / P. OttI. W. McBean (Dir.)

Lausanne, EPFL, 2014. DOI : 10.5075/epfl-thesis-6096.

Unsteady Aerodynamics of Low-Pressure Steam Turbines Operating Under Low Volume Flow

B. MegerleI. McBeanT. S. RiceP. Ott

Transactions- American Society of Mechanical Engineers Journal of Turbomachinery. 2014. DOI : 10.1115/1.4027373.

Hole Staggering Effect on the Cooling Performance of Narrow Impingement Channels Using the Transient Liquid Crystal Technique

A. TerzisG. WagnerJ. von WolfersdorfP. OttB. Weigand

Transactions- American Society of Mechanical Engineers Journal of Heat Transfer. 2014. DOI : 10.1115/1.4027250.

A Comparative Study of the Local Heat Transfer Distributions Around Various Surface Mounted Obstacles

R. WyssmannD. UllmerA. TerzisP. Ott

Journal of Thermal Science. 2014. DOI : 10.1007/s11630-014-0692-8.

Numerical and Experimental Investigations of an Annular Transonic Compressor Cascade Considering Leakage Flows

V. A. ChenauxM. BlocherP. Ott

2014. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-15), Honolulu, USA, February 24-28, 2014.

Local Heat Transfer Distributions of Small Impingement Configurations: A Detailed Experimental Procedure Using Transient Heat Transfer Methods

A. TerzisJ. von WolfersdorfB. WeigandP. Ott

2014. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-15), Honolulu, USA, February 24 - 28, 2014.

Experimental and numerical investigation of narrow impingement cooling channels

S. FechterA. TerzisP. OttB. WeigandJ. Von Wolfersdorf  et al.

International Journal Of Heat And Mass Transfer. 2013. DOI : 10.1016/j.ijheatmasstransfer.2013.09.003.

Experimental Aeroelastic Investigation of Vibrating Turbine Blade Clusters

A. ZankerP. OttP. Calza

18th Blade Mechanics Seminar, Winterthur, CH, September 11, 2013.

Unsteady Aerodynamics of Low-Pressure Steam Turbines Operating Under Low Volume Flow

B. MegerleT. S. RiceI. McBeanP. Ott

ANSYS Conference & 18th Swiss CADFEM Users‘ Meeting, Zurich, CH, September 05-06, 2013.

Experimental and Numerical Investigation of a Fully Confined Impingement Round Jet

O. CaggeseG. GnaegiG. HannemaA. TerzisP. Ott

International Journal of Heat and Mass Transfer. 2013. DOI : 10.1016/j.ijheatmasstransfer.2013.06.043.

Investigation of Flow Separation Control by Nanosecond Pulsed Dielectric Barrier Discharge Actuators

N. GrechP. PeschkeS. BustamenteP. LeylandP. Ott

2013. EUCCAS 2013 – 5th European Conference for Aeronautics and Space Sciences, Munich, Germany, July 1-5, 2013.

Experimental Investigation of Pulsed Dielectric Barrier Discharge Actuators in Sub- and Transonic Flow

P. PeschkeS. GoekceP. LeylandC. HollensteinP. Ott

2013. 44th AIAA Plasmadynamics and Lasers Conference, San Diego, CA, USA, June 24-27, 2013. DOI : 10.2514/6.2013-2885.

Experimental Aeroelastic Analysis of Clustered Turbine Blades Vibrating in Mixed Torsion/Bending Mode

A. ZankerP. OttP. Calza

2013. 31st AIAA Applied Aerodynamics Conference, San Diego, CA, USA, June 24-27, 2013. DOI : 10.2514/6.2013-3152.

Unsteady Aerodynamics of Low-Pressure Steam Turbines Operating Under Low Volume Flow

B. MegerleT. S. RiceI. McBeanP. Ott

2013. ASME Turbo Expo 2013, San Antonio, Texas, USA, June 3-7, 2013. DOI : 10.1115/GT2013-95409.

Evolution of the Aerodynamic Stability of an Oscillating Annular Compressor Cascade with Inlet Reverse Flow Condition Variations

V. ChenauxH. SchönenbornP. Ott

2013. ETC10 - 10th European Conference on Turbomachinery, Lappeenranta, FI, April 14-19, 2013. p. 907-916.

Experimental Aeroelastic Investigation of Vibrating Turbine Blade Clusters

A. ZankerP. OttP. Calza

2013. ETC10 - 10th European Conference on Turbomachinery, Lappeenranta, FI, April 14-19, 2013. p. 210-221.

High Voltage Pulsed DBD Effects on the Aerodynamic Performances and on the Shock Buffet

A. MarinoP. PeschkeF. De GregorioP. LeylandP. Ott  et al.

ERCOFTAC Bulletin. 2013.

Numerical and Experimental Investigation of the Aerodynamic Excitation of a Model Low-Pressure Steam Turbine Stage Operating Under Low Volume Flow

B. MegerleT. S. RiceI. W. McBeanP. Ott

Journal of Engineering for Gas Turbines and Power. 2013. DOI : 10.1115/1.4007334.

High Voltage Pulsed DBD Effects on the Aerodynamic Performances and on the Shock Buffet

A. MarinoP. PeschkeF. De GregorioP. LeylandP. Ott  et al.

Joint ERCOFTAC/PLASMAERO Public Workshop, Toulouse; F, December 10-12, 2012.

Thermocouple Thermal Inertia Effects on Impingement Heat Transfer Experiments Using the Transient Liquid Crystal Technique

A. TerzisJ. von WolfersdorfB. WeigandP. Ott

Measurement Science and Technology. 2012. DOI : 10.1088/0957-0233/23/11/115303.

Characterization of Kinetic Processes in Nano Pulsed SDBD

S. GoekceP. PeschkeC. HollensteinP. LeylandP. Ott

2012. NEPCAP 2012 - 5th International Symposium on "Non-Equilibrium Processes, Plasma, Combustion, and Atmospheric Phenomena", Sochi (Loo), RU, October 1-6, 2012.

Experimental Investigations of an Oscillating Annular Compressor Cascade at Reverse Flow Conditions

V. A. ChenauxH. SchönenbornP. Ott

2012. ISUAAAT13 - 13th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, Tokyo, JP, September 11-14, 2012.

Aerodynamic Excitation of a Model Low-Pressure Steam Turbine Stage Under Low Volume Flow

B. MegerleT. S. RiceI. W. McBeanP. Ott

17th Blade Mechanics Seminar, Winterthur, CH, September 12, 2012.

Investigation of High-Pressure Turbine Endwall Film-Cooling Performance Under Realistic Inlet Conditions

S. SalvadoriL. OttanelliM. JonssonP. OttF. Martelli

AIAA Journal of Propulsion and Power. 2012. DOI : 10.2514/1.59225.

Hole Staggering Effect on the Cooling Performance of Narrow Impingement Channels

A. TerzisG. WagnerP. Ott

2012. ASME Turbo Expo 2012 (GT2012), Copenhagen, DK, June 11-15, 2012. p. 127-138. DOI : 10.1115/GT2012-68323.

Numerical and Experimental Investigation of the Aerodynamic Excitation of a Model Low-Pressure Steam Turbine Stage Operating Under Low Volume Flow

B. MegerleT. S. RiceI. W. McBeanP. Ott

2012. ASME Turbo Expo 2012 (GT2012), Copenhagen, DK, June 11-15, 2012. p. 403-414. DOI : 10.1115/GT2012-68384.

Swirl Jets in Crossflow at Low Velocity Ratios

A. TerzisC. KazakosA. KalfasP. ZachosP. Ott

Journal of Mechanics Engineering and Automation. 2012.

Experimental Investigation of the Aeroelastic Stability of an Annular Compressor Cascade at Reverse Flow Conditions

V. A. Chenaux / P. Ott (Dir.)

Lausanne, EPFL, 2012. DOI : 10.5075/epfl-thesis-5358.

Heat Transfer and Performance Characteristics of Axial Cooling Fans with Downstream Guide Vanes

A. TerzisI. StylianouA. KalfasP. Ott

Journal of Thermal Science. 2012. DOI : 10.1007/s11630-012-0531-8.

Influence of Thermocouple Thermal Inertia in Impingement Heat Transfer Experiments Using Transient Techniques

A. TerzisJ. von WolfersdorfG. WagnerB. WeigandP. Ott

2012. XXI Biannual Symposium on Measuring Techniques in Turbomachinery, Valencia, E, March 22-23, 2012.

Investigation of High Pressure Turbine End-Wall Film Cooling Performances under Realistic Inlet Conditions

S. SalvadoriL. OttanelliM. JonssonF. MartelliP. Ott

2011. XX International Symposium on Air Breathing Engines (ISABE), Gothenburg, S, September 12-16, 2011.

Investigation on the Three-Dimensional Flow Mechanisms in Annular Axial Compressor Cascades for Aero Engines with Flow Control by Aspiration on the Hub and on the Blades

E. Colombo / P. Ott (Dir.)

Lausanne, EPFL, 2011. DOI : 10.5075/epfl-thesis-5241.

Effect of Stators on the Performance and the Thermal Capabilities of Small Axial Cooling Fans

A. TerzisI. StylianouA. KalfasP. Ott

2011. 10th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows (ISAIF-10), Brussels, Belgium, 4-7 July, 2011.

Interaction Between Nanosecond Pulse DBD Actuators and Transonic Flow

P. PeschkeS. GoekceC. HollensteinP. LeylandP. Ott

2011. 41st AIAA Fluid Dynamics Conference and Exhibit, Honolulu, HI, USA, June 27-40, 2011. DOI : 10.2514/6.2011-3734.

Aeroelasticity at Reversed Flow Conditions – Part 1: Numerical and Experimental Investigations of a Compressor Cascade with Controlled Vibration

H. SchönenbornV. ChenauxP. Ott

2011. ASME Turbo Expo 2011, Power for Land, Sea & Air, Vancouver, CAN, June 6-10, 2011. p. 1171-1181. DOI : 10.1115/GT2011-45034.

Electron temperature measurements using N2 and Argon transitions in an ATP fast pulsed DBD

S. GoekceP. PeschkeP. OttC. HollensteinP. Leyland

2011 Aerospace Thematic Workshop at Les Houches (Fundamentals of Aerodynamic Flow and Combustion Control by Plasmas), Les Houches, France, March 27 - April 01, 2011.

Experimental Investigations of the Aerodynamics of an Annular Compressor Cascade at Reversed Flow Conditions

V. ChenauxH. SchönenbornP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 249-259.

Swirl Jet and Crossflow Interaction at Low Velocity Ratios and Incompressible Flows

A. TerzisC. KazakosP. ZachosA. KalfasP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 133-144.

Influence of Blade Aspiration on the Flow Quality of an Annular Axial Compressor Cascade

E. ColomboL. CastillonP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 1345-1356.

Characterization of the Flow Generated in an Annular Test Facility

C. DeslotE. ColomboF. LeboeufD. CharbonnierP. Ott

2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, March 21-25, 2011. p. 1413-1424.

Investigation of End-Wall Film Cooling Configuration Performances in a Linear Cascade

S. SalvadoriL. OttanelliF. MartelliM. JonssonP. Ott

2010. 65° Congresso Nazionale ATI, Cagliari, Italy, September 13-17, 2010.

Aero Engine Flow Control by Surface Discharge Plasma

S. GoekceP. PeschkeC. HollensteinP. OttP. Leyland

2010. III International Scientific and Technical Conference - Aeroengines of XXI Century, Moscow, RU, November 30 - December 3, 2010.

Heat Transfer Measurements in a Turbine Cascade: Taking Advantage of the Thermal Bahaviour of a PSP Sensor

M. JonssonP. Ott

2010. XX Biannual Symposium on Measuring Techniques in Turbomachinery, Transonic and Supersonic Flow in Cascades and Turbomachines, Milano, Italy, September 23-24, 2010.

Surface DBD’s and plasma-flow interaction

S. GoekceP. PeschkeC. HollensteinP. LeylandP. Ott  et al.

2010. Euromech Fluid Mechanics Conference - 8, Bad Reichenhall, D, September 13-16, 2010.

Investigations on Axial Compressor Cascades with Aspiration on Blades and Hub

E. ColomboC. DeslotP. OttF. BarioL. Castillon  et al.

European Workshop on New Aero Engine Concepts, Munich, Germany, June 30-July 1, 2010.

Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling

M. Jonsson / P. Ott (Dir.)

Lausanne, EPFL, 2010. DOI : 10.5075/epfl-thesis-4650.

EPFL-LTT: Turbomachinery Laboratory

P. Ott

ERCOFTAC Bulletin. 2009.

Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform

D. CharbonnierP. OttM. JonssonF. CottierT. Köbke

2009. ASME Turbo Expo 2009, Orlando, Fl, USA, June 8-12, 2009. p. 1027-1038. DOI : 10.1115/GT2009-60306.

Effects of a surface dielectric barrier discharge on transonic flows around an airfoil

S. PavonP. OttP. LeylandJ.-L. DorierC. Hollenstein

2009. 47th AIAA Aerospace Sciences Meeting, Orlando, Florida, USA, January 05-08, 2009. DOI : 10.2514/6.2009-649.

Interaction between a surface dielectric barrier discharge and transonic airflows

S. Pavón / P. OttJ. R. Thome (Dir.)

Lausanne, EPFL, 2008. DOI : 10.5075/epfl-thesis-4201.

Comparison of Numerical Investigations With Measured Heat Transfer Performance of a Film Cooled Turbine Vane

D. CharbonnierP. OttM. JonssonT. KöbkeF. Cottier

2008. 53rd ASME Turbo Expo 2008, Berlin, Germany, June 9-13, 2008. p. 571-582. DOI : 10.1115/GT2008-50623.

Application of the Transient Heater Foil Technique for Heat Transfer and Film Cooling Effectiveness Measurements on a Turbine Vane Endwall

M. JonssonD. CharbonnierP. OttJ. von Wolfersdorf

2008. 53rd ASME Turbo Expo 2008, Berlin, Germany, June 9-13, 2008. p. 443-453. DOI : 10.1115/GT2008-50451.

Application of the Transient Heater Foil Technique for Heat Transfer Measurements

M. JonssonP. Ott

2008. XIX Biannual Symposium on Measuring Techniques in Turbomachinery, VKI, Rhode-St-Genèse, Belgium, April 7-8, 2008.

Numerical Analysis of Adiabatic Film Cooling Effectiveness Around HP-Turbine Airfoil – Decomposed Computation of Internal-External Airflows

D. CharbonnierM. JonssonP. Ott

2008. ISROMAC-12, Honolulu, Hawaii, USA, 17-22 February, 2008.

Leading Edge Film Cooling and the Influence of Fan Shaped Holes at Design and Off-Design Conditions

G. WagnerP. OttG. VogelS. Naik

2007. ASME Turbo Expo 2007, Montreal, Canada, May 14-17, 2007. p. 577-587. DOI : 10.1115/GT2007-27715.

Effects of high-speed airflows on a surface dielectric barrier discharge

S. Pavon-L. DorierC. HollensteinP. OttP. Leyland

Journal of Physics D : Applied Physics. 2007. DOI : 10.1088/0022-3727/40/6/021.

Heat Transfer Experiments on an Heavily Film Cooled Nozzle Guide Vane

M. JonssonP. Ott

2007. 7th European Turbomachinery Conference - ETC7, Athens, Greece, 5-9 March 2007. p. 1011-1020.

Analysis of the Cooling Performance on a Showerhead Cooled Blunt Body using the Wall Cooling Effectiveness

E. ColomboG. WagnerJ. von WolfersdorfP. Ott

2007. 7th European Turbomachinery Conference - ETC7, Athens, Greece, 5-9 March 2007. p. 989-998.

Experimental Investigation of Combined/Simultaneous Gust and Oscillating Turbine Row Unsteady Aerodynamics in Transonic Flow

A. BerettaF. RottmeierP. Ott

2007. 7th European Turbomachinery Conference - ETC7, Athens, Greece, 5-9 March 2007. p. 1285-1297.

Temperature and Pressure Sensitive Coatings

J. von WolfersdorfP. OttB. Weigand

Flow Phenomena in Nature, Volume 2 - Inspiration, Learning and Application; Southampton, UK: WIT Press, 2006. p. 747-766.

Experimental Investigations of Turbine Blade Showerhead Cooling

G. WagnerG. VogelP. Ott

2006. 13th International Heat Transfer Conference (IHTC-13), Sydney, Australia, August 13 - 18, 2006.

Influence of Mainstream Incidence Angle on Leading Edge Film Cooling Measured by the Transient Liquid Crystal Technique

G. WagnerP. OttG. Vogel

2006. 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-11), Honolulu, Hawaii, February 26 - March 2, 2006.

Effects of transonic air flows on a dielectric barrier discharge

S. Pavon-L. DorierC. HollensteinP. OttP. Leyland

2006. Gordon Research Conference on Plasma Processing Science (GRC-PPS), Mount Holyoke College, South Hadley, MA, July 16-21, 2006.

Experimental investigations on showerhead cooling on a blunt body

C. FalcozB. WeigandP. Ott

International Journal of Heat and Mass Transfer. 2006. DOI : 10.1016/j.ijheatmasstransfer.2005.10.012.

A comparative study on showerhead cooling performance

C. FalcozB. WeigandP. Ott

International Journal of Heat and Mass Transfer. 2006. DOI : 10.1016/j.ijheatmasstransfer.2005.10.013.

Combined/simultaneous gust and oscillating turbine row unsteady aerodynamics in subsonic flow

A. BerettaF. RottmeierP. Ott

Experimental Thermal and Fluid Science. 2006. DOI : 10.1016/j.expthermflusci.2005.09.001.

Influence of Modeshape Mistuning on the Forced Response of a Turbine Cascade

A. BerettaG. KahlP. Ott

2006. 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-11), Honolulu, Hawaii, February 26 - March 2, 2006.

Method for Analysis of Showerhead Film Cooling Experiments on Highly Curved Surfaces

G. WagnerE. SchneiderJ. v. WolfersdorfP. OttB. Weigand

2005. 6th European Turbomachinery Conference - ETC6, Lille, France, 7-11 March 2005. p. 381-389. DOI : 10.1016/j.expthermflusci.2006.05.006.

The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

G. WagnerM. KotullaP. OttB. WeigandJ. von Wolfersdorf

Journal of Turbomachinery. 2005. DOI : 10.1115/1.1811089.

Combined/Simultaneous Gust and Oscillating Turbine Row Unsteady Aerodynamics in Subsonic Flow

A. BerettaF. RottmeierP. Ott

2005.