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Documents dont l'auteur est "Vo, Huu Duc"

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Nombre de documents: 47

A

Ashrafi, F., & Vo, H. D. (2024). Passive flow control at impeller radial bend for stall delay in centrifugal compressors with fishtail pipe diffusers. Aerospace Science and Technology, 145, 108840 (23 pages). Lien externe

Ashrafi, F., & Vo, H. D. (juin 2018). Assessment of flow control strategies for improving centrifugal compressor efficiency [Communication écrite]. ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition (GT 2018), Oslo, Norway (11 pages). Lien externe

Akcayoz, E., Vo, H. D., & Mahallati, A. (2016). Controlling corner stall separation with plasma actuators in a compressor cascade. Journal of Turbomachinery, 138(8), 13 pages. Lien externe

Ashrafi, F., Michaud, M., & Vo, H. D. (2016). Delay of rotating stall in compressors using plasma actuators. Journal of Turbomachinery, 138(9), 12 pages. Lien externe

Akcayoz, E., Vo, H. D., & Mahallati, A. (juin 2015). Controlling corner stall separation with plasma actuators in a compressor cascade [Communication écrite]. ASME Turbo Expo : Turbine Technical Conference and Exposition (GT 2015), Montréal, Québec (11 pages). Lien externe

Ashrafi, F., Michaud, M., & Vo, H. D. (juin 2015). Delay of rotating stall in compressors using plasma actuators [Communication écrite]. ASME Turbo Expo : Turbine Technical Conference and Exposition (GT 2015), Montréal, Québec. Lien externe

B

Bagade, P. M., Sengupta, T. K., Sengupta, S., & Vo, H. D. (décembre 2014). Frequency Dependent Capacitance SDBD Plasma Model for Flow Control [Communication écrite]. IUTAM Symposium on Advances in Computation, Modeling and Control of Transitional and Turbulent Flows, Goa, India. Lien externe

Boesch, G., Vo, H. D., Savard, B., Wanko-Tchatchouang, C., & Mureithi, N. W. (2010). Flight Control Using Wing-Tip Plasma Actuation. Journal of Aircraft, 47(6), 1836-1846. Lien externe

C

Cevik, M., Vo, H. D., & Yu, H. (2016). Casing treatment for desensitization of compressor performance and stability to tip clearance. Journal of Turbomachinery, 138(12), 16 pages. Lien externe

D

Dammak, H., Versailles, P., & Vo, H. D. (2022). Coupled High Pressure-Temperature Effects on Performance of Dielectric Barrier Discharge Actuators. AIAA Journal, 60(6), 3917-3922. Lien externe

Dejour, Q., & Vo, H. D. (juin 2018). Assessment of a novel non-axial counter-rotating compressor concept for aero-engines [Communication écrite]. ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition (GT 2018), Oslo, Norway (9 pages). Lien externe

Djeghri, N., Vo, H. D., & Yu, H. (juin 2015). Parametric study for lossless casing treatment on a mixed-flow compressor rotor [Communication écrite]. ASME Turbo Expo : Turbine Technical Conference and Exposition (GT 2015), Montréal, Québec. Lien externe

Dumas, M., Vo, H. D., & Yu, H. (juin 2015). Post-surge load prediction for multi-stage compressors via CFD simulations [Communication écrite]. ASME Turbo Expo : Turbine Technical Conference and Exposition (GT 2015), Montréal, Québec. Lien externe

Drolet, M., Vo, H. D., & Mureithi, N. W. (2013). Effect of Tip Clearance on the Prediction of Nonsynchronous Vibrations in Axial Compressors. Journal of Turbomachinery, 135(1). Lien externe

Drolet, M., Vo, H. D., & Mureithi, N. W. Effect of Tip Clearance on the Prediction of Non-Synchronous Vibrations in Axial Compressors [Communication écrite]. ASME Turbo Expo. Lien externe

Drolet, M., Thomassin, J., Vo, H. D., & Mureithi, N. W. (juin 2009). Numerical Investigation Into Non-Synchronous Vibrations of Axial Flow Compressors by the Resonant Tip Clearance Flow [Communication écrite]. ASME Turbo Expo: Power for Land, Sea, and Air (GT 2009), Orlando, Florida, USA. Lien externe

E

Erler, E., Vo, H. D., & Yu, H. (2016). Desensitization of axial compressor performance and stability to tip clearance size. Journal of Turbomachinery, 138(3), 12 pages. Lien externe

Erler, E., Vo, H. D., & Yu, H. (juin 2015). Desensitization of axial compressor performance and stability to tip clearance size [Communication écrite]. ASME Turbo Expo : Turbine Technical Conference and Exposition (GT 2015), Montréal, Québec (14 pages). Lien externe

G

Gu, X., Vo, H. D., Mureithi, N. W., & Laurendeau, É. (2022). Plasma gurney flap flight control at low angle of attack. Journal of Aircraft, 60(1), 172-189. Lien externe

L

Liu, L., & Vo, H. D. (2024). Attenuation of Inlet Distortion Effects on Fans Using Asymmetric Inlet Guide Vanes. Journal of Turbomachinery, 23-1096 (33 pages). Lien externe

Lemire, S., & Vo, H. D. (2011). Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction. Journal of Turbomachinery, 133(1), 011017-011017. Lien externe

Lemire, S., Vo, H. D., & Benner, M. W. (2009). Performance improvement of axial compressors and fans with plasma actuation. International Journal of Rotating Machinery, 2009, 1-13. Disponible

M

Michaud, M., Milan, P., & Vo, H. D. (2016). Low-Cost Rotating Experimentation in Compressor Aerodynamics Using Rapid Prototyping. International Journal of Rotating Machinery, 2016, 1-10. Disponible

Milan, P., Demers, F., & Vo, H. D. (juin 2015). Modeling of saw-tooth DBD plasma actuators for flow control simulations [Communication écrite]. 45th AIAA Fluid Dynamics Conference, Dallas, TX, United states (11 pages). Lien externe

S

Souleimani, Y., Vo, H. D., & Yu, H. (juin 2018). Performance desensitization for a high-speed axial compressor [Communication écrite]. ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition (GT 2018), Oslo, Norway (14 pages). Lien externe

T

Thomassin, J., Mureithi, N. W., & Vo, H. D. (2014). Mixing layer resonance under high-speed stream forcing. Journal of Sound and Vibration, 333(24), 6453-6473. Lien externe

Thomassin, J., Vo, H. D., & Mureithi, N. W. (2011). The tip clearance flow resonance behind axial compressor nonsynchronous vibration. Journal of Turbomachinery, 133(4). Lien externe

Thomassin, J., Vo, H. D., & Mureithi, N. W. (2009). Blade Tip Clearance Flow and Compressor Nonsynchronous Vibrations: the Jet Core Feedback Theory as the Coupling Mechanism. Journal of Turbomachinery, 131(1). Lien externe

Thomassin, J., Vo, H. D., & Mureithi, N. W. (juin 2009). Experimental Demonstration of the Tip Clearance Flow Resonance Behind Compressor Non-Synchronous Vibration [Communication écrite]. ASME Turbo Expo: Power for Land, Sea and Air (GT 2008), Berlin, Germany. Lien externe

Thomassin, J., Vo, H. D., & Mureithi, N. W. (mai 2007). Blade Tip Clearance Flow and Compressor NSV: The Jet Core Feedback Theory as the Coupling Mechanism [Communication écrite]. ASME Turbo Expo: Power for Land, Sea and Air (GT 2007), Montreal, Qc, Canada. Lien externe

V

Vo, H. D., & Mureithi, N. W. (2018). Improving aircraft performance with plasma actuators. Lien externe

Vo, H. D., Cevik, M., & Erler, E. (2016). Compressor casing. (Demande de brevet no US20160040546). Lien externe

Vo, H. D., & Trépanier, J.-Y. (2016). Undergraduate Project in Compressor Rig Design, Fabrication, and Testing for Complete Engineering Training. Journal of Engineering for Gas Turbines and Power, 138(5), 13 pages. Lien externe

Vo, H. D., & Trépanier, J.-Y. (juin 2015). Undergraduate project in compressor rig design, fabrication and testing for complete engineering training [Communication écrite]. ASME Turbo Expo : Turbine Technical Conference and Exposition (GT 2015), Montréal, Québec. Lien externe

Vo, H. D. (2012). Apparatus and method for controlling a compressor. (Brevet no US8096756). Lien externe

Versailles, P., Chishty, W. A., & Vo, H. D. (2012). Application of Dielectric Barrier Discharge to Improve the Flashback Limit of a Lean Premixed Dump Combustor. Journal of Engineering for Gas Turbines and Power, 134(3), 8-8. Lien externe

Versailles, P., Ghosh, S., Vo, H. D., & Masson, C. (2011). Preliminary assessment of wind turbine blade lift control via plasma actuation. Wind Engineering, 35(3), 339-356. Lien externe

Versailles, P., Gingras-Gosselin, V., & Vo, H. D. (2010). Impact of pressure and temperature on the performance of plasma actuators. AIAA Journal, 48(4), 859-863. Lien externe

Vo, H. D. (2010). Role of tip clearance flow in rotating instabilities and nonsynchronous vibrations. Journal of Propulsion and Power, 26(3), 556-561. Lien externe

Vo, H. D. (2010). Rotating stall suppression in axial compressors with casing plasma actuation. Journal of Propulsion and Power, 26(4), 808-818. Lien externe

Vo, H. D., Cameron, J. D., & Morris, S. C. (juin 2008). Control of Short Length-Scale Rotating Stall Inception on a High-Speed Axial Compressor With Plasma Actuation [Communication écrite]. ASME Turbo Expo: Power for Land, Sea and Air (GT 2008), Berlin, Germany. Lien externe

Vo, H. D., Tan, C. S., & Greitzer, E. M. (2008). Criteria for spike initiated rotating stall. Journal of Turbomachinery, 130(1), 1-9. Lien externe

Vo, H. D. (2007). Active suppression of rotating stall inception with distributed jet actuation. International Journal of Rotating Machinery, 2007, 1-16. Disponible

Vo, H. D. (juin 2007). Control of rotating stall in axial compressors using plasma actuators [Communication écrite]. 37th AIAA Fluid Dynamics Conference, Miami, FL, United States. Lien externe

Vo, H. D. (mai 2007). Suppression of short length-scale rotating stall inception with glow discharge actuation [Communication écrite]. ASME Turbo Expo, Montréal, Québec. Lien externe

X

Xu, X. F., Vo, H. D., Mureithi, N. W., & Zhang, X. F. (novembre 2010). Turbulent Boundary Layer Separation Control by Using Dbd Plasma Actuators: Part I - Experimental Investigation [Communication écrite]. ASME International Mechanical Engineering Congress and Exposition (IMECE 2010), Vancouver, BC, Canada. Lien externe

Xu, X. F., Vo, H. D., Mureithi, N. W., & Zhang, X. F. (novembre 2010). Turbulent Boundary Layer Separation Control by Using Dbd Plasma Actuators: Part II - Numerical Model Validation and Parametric Study [Communication écrite]. ASME International Mechanical Engineering Congress and Exposition (IMECE 2010), Vancouver, BC, Canada. Lien externe

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