Département de génie mécanique
Axes de recherche :
- Aérospatial
Expertises :
- Aérodynamique
- Industrie 4.0
- Moteur d’avion
- Design conceptuel
- Système de propulsion
- Turbines
ÉTS
| AER600 | Introduction à l’aérospatiale | (Automne 2019) |
Système d'analyse de rotor pour turbine aéro, par Andruskiewitsch,Alexis.
Automne
2019
Turbine Rotors Parameters Definition, par Mesbah,Nacim.
Hiver
2012
En codirection avec : Garnier, François
Parametric Turbine Coverplate Analyzer at Preliminary Design Stage, par Guelin,Vincent.
Automne
2015
En codirection avec : levy, Stephane
New Engine Development Validation - Gas Turbine Product System, par Postec,Camille.
Automne
2015
PDDS - Rotor Dynamics, par Kelly,Jean-Daniel.
Hiver
2020
Intégration des données historiques dans les activités de digitalisation : comment migrer avec succès des données historiques dans les activités de digitalisation futures, par Oulai,Jean Grace.
Hiver
2020
Développement d'un logiciel permettant l'assemblage de l'étage haute pression d'un moteur industriel, par Galopeau,Raphaël.
Hiver
2019
Développement d'un algorithme de stacking automatisé pour l'alignement des blades de rotor, par Laviec,Florian.
Été
2019
PDDS - Blade Shroud Module, par Postec,Camille.
Automne
2015
Measurement of the Wall Shear Stress in an Adverse Pressure Gradient Boundary Layer, par Lemaire,Thomas.
Été
2017
Système d'analyse de rotor pour turbine aéro, par Andruskiewitsch,Alexis.
Automne
2019
Implantation du module Rotor Dynamics, par Kelly,Jean-Daniel.
Hiver
2020
Intégration du modèle de performance thermodynamique d'une turbine à gaz à une plateforme d'optimisation de design multidisciplinaire, par Audéon,Baptiste.
Automne
2018
Amélioration des processus de gestion du développement de la technologie, par Lamin,Ilia.
Été
2020
En codirection avec : Blondin, Benoit
Platform for the preliminary design of a disc in a compressor rotor, par Aubery,Claire-Wêndbenedo.
Été
2020
En codirection avec : Staniszewski, Martin
Digital Multidisciplinary Analysis and Design Optimization DMADO Platform for Aeroderivative Gas Turbines, par Camirand,William.
Hiver
2020
En codirection avec : Doran, Pascal
Propulsion System Integration and Optimization, par Bérard,Florence.
Été
2020
Single Platform Simulation Tool for Turbine Disc Design and Analysis at Preliminary Design Stage, par Lagloire,François.
Automne
2013
En codirection avec : Blondin, Benoit
Digital Multidisciplinary Analysis and Design Optimization (DMADO) Platform for Aero Derivate Gas Turbine, par Ousseni,Hicham Faissoil.
Automne
2018
Digital Multidisciplinary Analysis and Design Optimization "DMADO" Platform for Aeroderivative Gas Turbines, par Paramassivam,Nadia.
Hiver
2020
Intégration et optimisation du système de propulsion "PSIO", par Martin,Salomé.
Hiver
2020
En codirection avec : Garnier, François
Rapid Airfoil Design for Uncooled High Pressure Turbine Blades, par Moradi-Khaniabadi,Niloofar.
Automne
2015
En codirection avec : Garnier, François
Conception préliminaire de disques de turbine axiale pour moteurs d'aéronefs, par Ouellet,Yannick.
Hiver
2013
En codirection avec : Garnier, François
New Correlations for High-pressure Gas Turbine Housing and Shroud Segments, par Savaria,Christian.
Automne
2015
En codirection avec : Garnier, François
Turbine Blade Tip Leakage Loss Investigation, par Abou Salem,Ayman.
Été
2016
En codirection avec : Garnier, François
Automation & Integration of Secondary Air System Workflow for Multidisciplinary Design Optimization of Gas Turbines, par Peoch,Timothé.
Automne
2019
Développement d'un logiciel permettant la distribution d'aubes autour d'un rotor haute pression, par Galopeau,Raphaël.
Hiver
2019
Définir l'architecture avionique pour l'hélicoptère à turbine Winner B150, par Pedneault-Plourde,Nicola.
Été
2013
Développement et utilisation du système préliminaire de conception des turbomachines MOPEDS, par Breton,Jérémy.
Hiver
2017
Introduction aux outils de conception préliminaire pour les moteurs d'avion civil, par Lucchesi,Julian.
Été
2017
Study of Inner Air Seal Cavities : Mass Flow Balance Analysis and Heat Transfer Coefficient, par Lemaire,Thomas.
Été
2017
Marinisation de la turbine aérodérivative TRENT 60, par Samieri,Valério.
Hiver
2017
Optimization of a Predesign Tool, par Poncin-Dubé,Maxime.
Automne
2017
PW800 nacelle intégration coordination, par Villanueva,Lucas.
Été
2019
Rapport de stage industriel (MGA902), par Laviec,Florian.
Été
2019
En codirection avec : Moustapha, Saïd Hany
CFD Simulation of a Gas Turbine Combustor, par Saleh,Mohamed Elbayoumi.
Été
2020
En codirection avec : Garnier, François
Automation of a Turbine Tip Clearance Preliminary Calculation Process, par Moret,Maxime.
Été
2018
En codirection avec : Doré, Sylvie
Rapid Design Exploration of Turbine Blades at the Preliminary Design Stage, par Twahir,Abdul Halim.
Hiver
2020
En codirection avec : Moustapha, Saïd Hany
Advanced Conrol of Gas Turbine Engines, par Ibrahem,Ibrahem Mohamed Atia.
Été
2020
En codirection avec : Richard, Frédérique
Opérationnalisation du processus d'intelligence économique, par Ouboua,Houda.
Été
2014
En codirection avec : Iarusso, Giovanni
Optimisation du processus des réparations des moteurs d'avions, par Ait Ameur Meziane,Abdelkrim.
Hiver
2016
Ibrahem M. A. Ibrahem, Ouassima Akhrif, Hany Moustapha, Martin Staniszewski. 2019. « Neural networks modelling of aero-derivative gas turbine engine: a comparison study ». Proceedings of the 16th International Conference on Informatics in Control, Automation and Robotics (ICINCO) (Prague, Czech Republic, July 29-31, 2019) p. 738-745. SciTePress.
Ibrahem M. A. Ibrahem, Ouassima Akhrif, Hany Moustapha, Martin Staniszewski. 2019. « Neural networks modelling of aero-derivative gas turbine engine: a comparison study ». Proceedings of the 16th International Conference on Informatics in Control, Automation and Robotics (ICINCO) (Prague, Czech Republic, July 29-31, 2019) p. 738-745. SciTePress.
Pascal Doran, Ed Vlasic, Grant Guevremont, Hany Moustapha. 2018. « Gas-path optimization using turbine aerodynamics meanline and design exploration ». Proceedings of GPPS Society Forum 18 (Montréal, QC, Canada, May 07-09, 2018) Global Power and Propulsion Society.
Maxime Moret, François Garnier, Patricia Phutthavong, Hany Moustapha. 2018. « Automation of a turbine tip clearance preliminary calculation process ». Proceedings of GPPS Society Forum 18 (Montréal, QC, Canada, May 07-09, 2018) Global Power and Propulsion Society.
Pascal Doran, Ed Vlasic, Grant Guevremont, Hany Moustapha. 2018. « Gas-path optimization using turbine aerodynamics meanline and design exploration ». Proceedings of GPPS Society Forum 18 (Montréal, QC, Canada, May 07-09, 2018) Global Power and Propulsion Society.
Maxime Moret, François Garnier, Patricia Phutthavong, Hany Moustapha. 2018. « Automation of a turbine tip clearance preliminary calculation process ». Proceedings of GPPS Society Forum 18 (Montréal, QC, Canada, May 07-09, 2018) Global Power and Propulsion Society.
Abdulhalim Twahir, Hany Moustapha, Sylvie Doré, François Roy. 2017. « A framework for an integrated turbine rotor design system ». Global Power and Propulsion Forum : Proceedings (Zurich, Switzerland, Jan. 16-18, 2017) Global Power & Propulsion Society.
Abdulhalim Twahir, Hany Moustapha, Sylvie Doré, François Roy. 2017. « A framework for an integrated turbine rotor design system ». Global Power and Propulsion Forum : Proceedings (Zurich, Switzerland, Jan. 16-18, 2017) Global Power & Propulsion Society.
Maxime Moret, Alexandre Delecourt, Hany Moustapha, François Garnier, Acher-Igal Abenhaim. 2016. « Automated thermal and stress preliminary analyses applied to a turbine rotor ». ASME Turbo Expo : Turbomachinery Technical Conference and Exposition (Seoul, South Korea, June 13-17, 2016) ASME International.
Christian Savaria, François Garnier, Hany Moustapha, Patricia Phutthavong. 2016. « New correlations for high-pressure turbine housing and shroud segments ». ASME Turbo Expo : Turbomachinery Technical Conference and Exposition (Seoul, South Korea, June 13-17, 2016) ASME International.
Maxime Moret, Alexandre Delecourt, Hany Moustapha, François Garnier, Acher-Igal Abenhaim. 2016. « Automated thermal and stress preliminary analyses applied to a turbine rotor ». ASME Turbo Expo : Turbomachinery Technical Conference and Exposition (Seoul, South Korea, June 13-17, 2016) ASME International.
Christian Savaria, François Garnier, Hany Moustapha, Patricia Phutthavong. 2016. « New correlations for high-pressure turbine housing and shroud segments ». ASME Turbo Expo : Turbomachinery Technical Conference and Exposition (Seoul, South Korea, June 13-17, 2016) ASME International.
Niloofar Moradi, Edward Vlasic, Hany Moustapha. 2015. « Rapid airfoil design for uncooled high pressure turbine blades ». ASME Turbo Expo 2015: Turbine Technical Conference and Exposition (Montreal, QC, Canada, June 15-19, 2015) American Society of Mechanical Engineers (ASME).
Maxime Moret, Hany Moustapha, François Garnier, Acher-Igal Abenhaim. 2015. « Automatic thermal and stress preliminary analyses applied to a turbine rotor ». 62nd CASI Aeronautics Conference and AGM 3rd GARDN (Montreal, QC, Canada, May 19-21, 2015) CASI.
Niloofar Moradi, Edward Vlasic, Hany Moustapha. 2015. « Rapid airfoil design for uncooled high pressure turbine blades ». ASME Turbo Expo 2015: Turbine Technical Conference and Exposition (Montreal, QC, Canada, June 15-19, 2015) American Society of Mechanical Engineers (ASME).
Maxime Moret, Hany Moustapha, François Garnier, Acher-Igal Abenhaim. 2015. « Automatic thermal and stress preliminary analyses applied to a turbine rotor ». 62nd CASI Aeronautics Conference and AGM 3rd GARDN (Montreal, QC, Canada, May 19-21, 2015) CASI.
Yannick Ouellet, François Garnier, François Roy, Hany Moustapha. 2014. « A Preliminary Design System for Turbine Discs ». ASME Turbo Expo 2014: Turbine Technical Conference and Exposition (Düsseldorf, Germany, June 16–20, 2014) ASME.
Abdulhalim Twahir, Magdy Attia, Franois Roy, Hany Moustapha. 2014. « Preliminary design and analysis tool for aeroengine turbine fixings ». ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) (Montreal, QC, Canada, Nov. 14-20, 2014) American Society of Mechanical Engineers (ASME).
Yannick Ouellet, François Garnier, François Roy, Hany Moustapha. 2014. « A Preliminary Design System for Turbine Discs ». ASME Turbo Expo 2014: Turbine Technical Conference and Exposition (Düsseldorf, Germany, June 16–20, 2014) ASME.
Abdulhalim Twahir, Magdy Attia, Franois Roy, Hany Moustapha. 2014. « Preliminary design and analysis tool for aeroengine turbine fixings ». ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) (Montreal, QC, Canada, Nov. 14-20, 2014) American Society of Mechanical Engineers (ASME).
Benoit Blondin, François Lagloire, Hany Moustapha, Yannick Ouellet. 2013. « Single platform integration enviroment for turbine rotor design and analysis ». XXI International Symposium on Air Breathing Engines (ISABE) (Busan, Korea, Sept. 09-13, 2013) p. 1148-1156. AIAA.
Y. Ouellet, F. Roy, H. Moustapha, F. Garnier. 2013. « Preliminary design of axial turbine disc for aicraft engines ». CASI 60th aeronautic conference (Toronto, ON, Canada, Apr. 30-May 02, 2013) CASI.
Benoit Blondin, François Lagloire, Hany Moustapha, Yannick Ouellet. 2013. « Single platform integration enviroment for turbine rotor design and analysis ». XXI International Symposium on Air Breathing Engines (ISABE) (Busan, Korea, Sept. 09-13, 2013) p. 1148-1156. AIAA.
Y. Ouellet, F. Roy, H. Moustapha, F. Garnier. 2013. « Preliminary design of axial turbine disc for aicraft engines ». CASI 60th aeronautic conference (Toronto, ON, Canada, Apr. 30-May 02, 2013) CASI.
Sergey Andronenko, Ion Stiharu, Muthukuruman Packirisamy, Hany Moustapha, Patrice Dionne. 2005. « The use of microelectromechanical systems for surge detection in gas turbine engines ». Proceedings - 2005 International Conference on MEMS, NANO and Smart Systems (ICMENS) (Banff, AB, Canada, July 24-27, 2006) p. 355-358. Institute of Electrical and Electronics Engineers Computer Society.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2005. « An empirical prediction method for secondary losses in turbines: Part I - A new loss breakdown scheme and penetration depth correlation ». ASME Turbo Expo 2005: Power for Land, Sea, and Air (Reno, NV, USA, June 06-09, 2005) p. 625-635. ASME.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2005. « An empirical prediction method for secondary losses in turbines: Part II - A new secondary loss correlation ». ASME Turbo Expo 2005: Power for Land, Sea, and Air (Reno, NV, USA, June 06-09, 2005) p. 637-649. ASME.
Sergey Andronenko, Ion Stiharu, Muthukuruman Packirisamy, Hany Moustapha, Patrice Dionne. 2005. « The use of microelectromechanical systems for surge detection in gas turbine engines ». Proceedings - 2005 International Conference on MEMS, NANO and Smart Systems (ICMENS) (Banff, AB, Canada, July 24-27, 2006) p. 355-358. Institute of Electrical and Electronics Engineers Computer Society.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2005. « An empirical prediction method for secondary losses in turbines: Part I - A new loss breakdown scheme and penetration depth correlation ». ASME Turbo Expo 2005: Power for Land, Sea, and Air (Reno, NV, USA, June 06-09, 2005) p. 625-635. ASME.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2005. « An empirical prediction method for secondary losses in turbines: Part II - A new secondary loss correlation ». ASME Turbo Expo 2005: Power for Land, Sea, and Air (Reno, NV, USA, June 06-09, 2005) p. 637-649. ASME.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2004. « Measurements of secondary flows downstream of a turbine cascade at off-design incidence ». Proceedings of the ASME Turbo Expo 2004 (Vienna, Austria, June 14-17, 2004) p. 1299-1311. ASME.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2004. « Measurements of secondary flows downstream of a turbine cascade at off-design incidence ». Proceedings of the ASME Turbo Expo 2004 (Vienna, Austria, June 14-17, 2004) p. 1299-1311. ASME.
M. W. Banner, S. A. Sjolander, S. H. Moustapha. 2003. « The influence of leading-edge geometry on secondary losses in a turbine cascade at the design incidence ». ASME Turbo Expo 2003 (Atlanta, GA, USA, June 16-19, 2003) p. 147-161. ASME.
Hany Moustapha. 2003. « Future technology challenges for small gas turbines ». AIAA International Air and Space Symposium and Exposition: The Next 100 Years (Dayton, OH, 2003, July 14-17, 2003) AIAA.
M. W. Banner, S. A. Sjolander, S. H. Moustapha. 2003. « The influence of leading-edge geometry on secondary losses in a turbine cascade at the design incidence ». ASME Turbo Expo 2003 (Atlanta, GA, USA, June 16-19, 2003) p. 147-161. ASME.
Hany Moustapha. 2003. « Future technology challenges for small gas turbines ». AIAA International Air and Space Symposium and Exposition: The Next 100 Years (Dayton, OH, 2003, July 14-17, 2003) AIAA.
S. Girgis, E. Vlasic, J. P. Lavoie, S. H. Moustapha. 2002. « The effect of secondary air injection on the performance of a transonic turbine stage ». ASME Turbo Expo 2002: Power for Land, Sea, and Air (Amsterdam, The Netherlands, June 03-06, 2002) p. 147-157.
S. Girgis, E. Vlasic, J. P. Lavoie, S. H. Moustapha. 2002. « The effect of secondary air injection on the performance of a transonic turbine stage ». ASME Turbo Expo 2002: Power for Land, Sea, and Air (Amsterdam, The Netherlands, June 03-06, 2002) p. 147-157.
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2001. « Midspan flow-field measurements for two transonic linear turbine cascades at off-design conditions ». ASME Turbo Expo 2001: Power for Land, Sea, and Air (New Orleans, LA, USA, June 4-7, 2001) American Society of Mechanical Engineers (ASME).
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2001. « Midspan flow-field measurements for two transonic linear turbine cascades at off-design conditions ». ASME Turbo Expo 2001: Power for Land, Sea, and Air (New Orleans, LA, USA, June 4-7, 2001) American Society of Mechanical Engineers (ASME).
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2000. « Aerodynamic performance of a transonic turbine cascade at off-design conditions ». ASME Turbo Expo 2000: Power for Land, Sea, and Air (Munich, Germany, May 08-11, 2000) ASME.
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2000. « Aerodynamic performance of a transonic turbine cascade at off-design conditions ». ASME Turbo Expo 2000: Power for Land, Sea, and Air (Munich, Germany, May 08-11, 2000) ASME.
W. G. Habashi, M. P. Robichaud, S. H. Moustapha, G. J. Guèvremont, M. F. Peeters. 1999. « A practical and effective approach to cfd education, through a university-industry 1technology exchange perspective ». 37th Aerospace Sciences Meeting and Exhibit (Reno, NV, USA, Jan. 11-14, 1999) AIAA.
W. G. Habashi, M. P. Robichaud, S. H. Moustapha, G. J. Guèvremont, M. F. Peeters. 1999. « A practical and effective approach to cfd education, through a university-industry 1technology exchange perspective ». 37th Aerospace Sciences Meeting and Exhibit (Reno, NV, USA, Jan. 11-14, 1999) AIAA.
M. Woinowsky-Krieger, J. P. Lavoie, E. P. Vlasic, S. H. Moustapha. 1998. « Off-design performance of a single stage transonic turbine ». ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition (Stockholm, Sweden, June 02-05, 1998) ASME.
M. Woinowsky-Krieger, J. P. Lavoie, E. P. Vlasic, S. H. Moustapha. 1998. « Off-design performance of a single stage transonic turbine ». ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition (Stockholm, Sweden, June 02-05, 1998) ASME.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 1997. « Measurements of secondary flows in a turbine cascade at off-design incidence ». ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition (Orlando, FL, USA, June 02-05, 1997)
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 1997. « Measurements of secondary flows in a turbine cascade at off-design incidence ». ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition (Orlando, FL, USA, June 02-05, 1997)
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 1995. « Influence of leading-edge geometry on profile losses in turbines at off-design incidence: Experimental results and an improved correlation ». ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition, GT 1995 (Houston, TX, USA, June 05-08, 1995) ASME.
E. P. Vlasic, S. Girgis, S. H. Moustapha. 1995. « The design and performance of a high work research turbine ». ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition (Houston, TX, USA, June 05-08, 1995)
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 1995. « Influence of leading-edge geometry on profile losses in turbines at off-design incidence: Experimental results and an improved correlation ». ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition, GT 1995 (Houston, TX, USA, June 05-08, 1995) ASME.
E. P. Vlasic, S. Girgis, S. H. Moustapha. 1995. « The design and performance of a high work research turbine ». ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition (Houston, TX, USA, June 05-08, 1995)
M. Badger, A. Julien, A. D. LeBlanc, S. H. Moustapha, A. Prabhu, A. A. Smailys. 1993. « The PT6 engine: 30 years of gas turbine technology evolution ». ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993 (Cincinnati, OH, USA, May 24-27, 1993) ASME.
M. Badger, A. Julien, A. D. LeBlanc, S. H. Moustapha, A. Prabhu, A. A. Smailys. 1993. « The PT6 engine: 30 years of gas turbine technology evolution ». ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993 (Cincinnati, OH, USA, May 24-27, 1993) ASME.
S. H. Moustapha, W. E. Carscallen, J. D. McGeachy. 1992. « Aerodynamic performance of a transonic low aspect ratio turbine nozzle ». ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992 (Cologne, Germany, June 01-04, 1992) ASME.
P. Rodger, S. A. Sjolander, S. H. Moustapha. 1992. « Establishing two-dimensional flow in a large-scale planar turbine cascade ». AIAA/ASME/SAE/ASEE 28th Joint Propulsion Conference and Exhibit (Nashville, TN, USA, July 6-8, 1992) AIAA.
S. H. Moustapha, W. E. Carscallen, J. D. McGeachy. 1992. « Aerodynamic performance of a transonic low aspect ratio turbine nozzle ». ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992 (Cologne, Germany, June 01-04, 1992) ASME.
P. Rodger, S. A. Sjolander, S. H. Moustapha. 1992. « Establishing two-dimensional flow in a large-scale planar turbine cascade ». AIAA/ASME/SAE/ASEE 28th Joint Propulsion Conference and Exhibit (Nashville, TN, USA, July 6-8, 1992) AIAA.
B. Tremblay, S. A. Sjolander, S. H. Moustapha. 1990. « Off-Design performance of a linear cascade of turbine blades ». ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition (Brussels, Belgium, June 11–14, 1990) ASME.
B. Tremblay, S. A. Sjolander, S. H. Moustapha. 1990. « Off-Design performance of a linear cascade of turbine blades ». ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition (Brussels, Belgium, June 11–14, 1990) ASME.
S. H. Moustapha, S. C. Kacker, B. Tremblay. 1989. « An improved incidence losses prediction method for turbine airfoils ». ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition (Toronto, ON, Canada, June 04-08, 1989) ASME.
U. W. Schaub, R. G. Williamson, J. P. Huot, S. H. Moustapha. 1989. « An experimental assessment of the influence of downstream conditions on the performance of a transonic turbine nozzle of high turning ». ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition (Toronto, ON, Canada, June 04-08, 1989) ASME.
S. H. Moustapha, S. C. Kacker, B. Tremblay. 1989. « An improved incidence losses prediction method for turbine airfoils ». ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition (Toronto, ON, Canada, June 04-08, 1989) ASME.
U. W. Schaub, R. G. Williamson, J. P. Huot, S. H. Moustapha. 1989. « An experimental assessment of the influence of downstream conditions on the performance of a transonic turbine nozzle of high turning ». ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition (Toronto, ON, Canada, June 04-08, 1989) ASME.
S. H. Moustapha, G. J. Paron, J. H. T. Wade. 1985. « Secondary flow in cascades of highly loaded turbine blades ». 30th International Gas Turbine Conference and Exhibit (Houston, TX, USA, ) American Society of Mechanical Engineers.
S. H. Moustapha, R. G. Williamson. 1985. « Investigation of the effect of two endwall contours on the performance of an annular nozzle cascade ». 21st Joint Propulsion Conference (Monterey, CA, USA, July 08-11, 1985) AIAA.
R. G. Williamson, S. H. Moustapha. 1985. « Three-dimensional cascade testing of turbine nozzles at high exit mach numbers ». Three Dimensional Flow Phenomena in Fluid Machinery presented at the Winter Annual Meeting of the American Society of Mechanical Engineers (Miami Beach, FL, USA, Nov. 17-22, 1985) p. 45-54. ASME.
S. H. Moustapha, G. J. Paron, J. H. T. Wade. 1985. « Secondary flow in cascades of highly loaded turbine blades ». 30th International Gas Turbine Conference and Exhibit (Houston, TX, USA, ) American Society of Mechanical Engineers.
S. H. Moustapha, R. G. Williamson. 1985. « Investigation of the effect of two endwall contours on the performance of an annular nozzle cascade ». 21st Joint Propulsion Conference (Monterey, CA, USA, July 08-11, 1985) AIAA.
R. G. Williamson, S. H. Moustapha. 1985. « Three-dimensional cascade testing of turbine nozzles at high exit mach numbers ». Three Dimensional Flow Phenomena in Fluid Machinery presented at the Winter Annual Meeting of the American Society of Mechanical Engineers (Miami Beach, FL, USA, Nov. 17-22, 1985) p. 45-54. ASME.
S. A. El Shammaa, S. H. Moustapha, J. H. T. Wade. 1984. « Secondary flow in cascades of high turning angle turbine blades ». First Parsons International Turbine Conference (Dublin, Ireland, June 28-29, 1984) p. 93-104. Dublin, Ireland : Parsons Press.
S. A. El Shammaa, S. H. Moustapha, J. H. T. Wade. 1984. « Secondary flow in cascades of high turning angle turbine blades ». First Parsons International Turbine Conference (Dublin, Ireland, June 28-29, 1984) p. 93-104. Dublin, Ireland : Parsons Press.
Yannick Ouellet, Christian Savaria, François Roy, Hany Moustapha, François Garnier. 2019. « A Preliminary design system for turbine discs ». International Journal of Turbo & Jet-Engines. vol. 36 , nº 3. p. 329-338.
Yannick Ouellet, Christian Savaria, François Roy, Hany Moustapha, François Garnier. 2019. « A Preliminary design system for turbine discs ». International Journal of Turbo & Jet-Engines. vol. 36 , nº 3. p. 329-338.
C. Savaria, P. Phutthavong, H. Moustapha, F. Garnier. 2018. « Preliminary design for turbine housing and shroud segments ». Aeronautical Journal. vol. 122 , nº 1248. p. 260-282.
C. Savaria, P. Phutthavong, H. Moustapha, F. Garnier. 2018. « Preliminary design for turbine housing and shroud segments ». Aeronautical Journal. vol. 122 , nº 1248. p. 260-282.
Maxime Moret, Alexandre Delecourt, Hany Moustapha, Acher-Igal Abenhaim, Francois Garnier. 2017. « Automated thermal and stress preliminary analyses applied to a turbine rotor ». Aerospace Science and Technology. vol. 63 p. 123-131.
Maxime Moret, Alexandre Delecourt, Hany Moustapha, Acher-Igal Abenhaim, Francois Garnier. 2017. « Automated thermal and stress preliminary analyses applied to a turbine rotor ». Aerospace Science and Technology. vol. 63 p. 123-131.
François Lagloire, Yannick Ouellet, Benoit Blondin, François Garnier, Hany Moustapha. 2014. « Single platform integration environment for turbine rotor design and analysis ». Journal of Energy and Power Engineering. vol. 8 , nº 9. p. 1590-1598.
Nacim Mesbah, Sandy Seifert, Bruno Chatelois, François Garnier, Hany Moustapha. 2014. « Parameterization modeling of a gas turbine coverplate ». Journal of Energy and Power Engineering. vol. 9 , nº 8. p. 1378-1385.
François Lagloire, Yannick Ouellet, Benoit Blondin, François Garnier, Hany Moustapha. 2014. « Single platform integration environment for turbine rotor design and analysis ». Journal of Energy and Power Engineering. vol. 8 , nº 9. p. 1590-1598.
Nacim Mesbah, Sandy Seifert, Bruno Chatelois, François Garnier, Hany Moustapha. 2014. « Parameterization modeling of a gas turbine coverplate ». Journal of Energy and Power Engineering. vol. 9 , nº 8. p. 1378-1385.
Michael W. Benner, S. A. Sjolander, S. H. Moustapha. 2006. « An empirical prediction method for secondary losses in turbines - Part I: A new loss breakdown scheme and penetration depth correlation ». Journal of Turbomachinery. vol. 128 , nº 2. p. 273-280.
Michael W. Benner, S. A. Sjolander, S. H. Moustapha. 2006. « An empirical prediction method for secondary losses in turbines - Part II: A new secondary loss correlation ». Journal of Turbomachinery. vol. 128 , nº 2. p. 281-291.
Michael W. Benner, S. A. Sjolander, S. H. Moustapha. 2006. « An empirical prediction method for secondary losses in turbines - Part I: A new loss breakdown scheme and penetration depth correlation ». Journal of Turbomachinery. vol. 128 , nº 2. p. 273-280.
Michael W. Benner, S. A. Sjolander, S. H. Moustapha. 2006. « An empirical prediction method for secondary losses in turbines - Part II: A new secondary loss correlation ». Journal of Turbomachinery. vol. 128 , nº 2. p. 281-291.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2004. « The influence of leading-edge geometry on secondary losses in a turbine cascade at the design incidence ». Journal of Turbomachinery. vol. 126 , nº 2. 11 p. p. 277-287.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 2004. « The influence of leading-edge geometry on secondary losses in a turbine cascade at the design incidence ». Journal of Turbomachinery. vol. 126 , nº 2. 11 p. p. 277-287.
Iyad Akel, Wagdi G. Habashi, Hany S. Moustapha. 2002. « Toward CFD-based correlations for single-stage high-pressure transonic turbine stage ». International Journal of Rotating Machinery. vol. 8 , nº 5. p. 337-352.
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2002. « Midspan flow-field measurements for two transonic linear turbine cascades at off-design conditions ». Journal of Turbomachinery. vol. 124 , nº 2. p. 176-186.
Iyad Akel, Wagdi G. Habashi, Hany S. Moustapha. 2002. « Toward CFD-based correlations for single-stage high-pressure transonic turbine stage ». International Journal of Rotating Machinery. vol. 8 , nº 5. p. 337-352.
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2002. « Midspan flow-field measurements for two transonic linear turbine cascades at off-design conditions ». Journal of Turbomachinery. vol. 124 , nº 2. p. 176-186.
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2001. « Aerodynamic performance of a transonic turbine cascade at off-design conditions ». Journal of Turbomachinery. vol. 123 , nº 3. p. 510-518.
D. B. M. Jouini, S. A. Sjolander, S. H. Moustapha. 2001. « Aerodynamic performance of a transonic turbine cascade at off-design conditions ». Journal of Turbomachinery. vol. 123 , nº 3. p. 510-518.
M. Woinowsky-Krieger, J. P. Lavoie, E. P. Vlasic, S. H. Moustapha. 1999. « Off-design performance of a single-stage transonic turbine ». Journal of Turbomachinery. vol. 121 , nº 2. p. 177-183.
M. Woinowsky-Krieger, J. P. Lavoie, E. P. Vlasic, S. H. Moustapha. 1999. « Off-design performance of a single-stage transonic turbine ». Journal of Turbomachinery. vol. 121 , nº 2. p. 177-183.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 1997. « Influence of leading-edge geometry on profile losses in turbines at off-design incidence: Experimental results and an improved correlation ». Journal of Turbomachinery. vol. 119 , nº 2. p. 193-200.
M. W. Benner, S. A. Sjolander, S. H. Moustapha. 1997. « Influence of leading-edge geometry on profile losses in turbines at off-design incidence: Experimental results and an improved correlation ». Journal of Turbomachinery. vol. 119 , nº 2. p. 193-200.
E. P. Vlasic, S. Girgis, S. H. Moustapha. 1996. « The design and performance of a high work research turbine ». Journal of Turbomachinery. vol. 118 , nº 4. p. 792-799.
E. P. Vlasic, S. Girgis, S. H. Moustapha. 1996. « The design and performance of a high work research turbine ». Journal of Turbomachinery. vol. 118 , nº 4. p. 792-799.
M. Badger, A. Julien, A. D. LeBlanc, S. H. Moustapha, A. Prabhu, A. A. Smailys. 1994. « The PT6 engine: 30 years of gas turbine technology evolution ». Journal of Engineering for Gas Turbines and Power. vol. 116 , nº 2. p. 322-330.
M. Badger, A. Julien, A. D. LeBlanc, S. H. Moustapha, A. Prabhu, A. A. Smailys. 1994. « The PT6 engine: 30 years of gas turbine technology evolution ». Journal of Engineering for Gas Turbines and Power. vol. 116 , nº 2. p. 322-330.
S. H. Moustapha, W. E. Carscallen, J. D. McGeachy. 1993. « Aerodynamic performance of a transonic low aspect ratio turbine nozzle ». Journal of Turbomachinery. vol. 115 , nº 3. p. 400-408.
D. R. Whitehouse, S. H. Moustapha, S. A. Sjolander. 1993. « Effect of axial velocity ratio, turbulence intensity, incidence, and leading edge geometry on the midspan performance of a turbine cascade ». Canadian Aeronautics and Space Journal = Journal Aéronautique et Spatial du Canada. vol. 39 , nº 3. p. 150-156.
S. H. Moustapha, W. E. Carscallen, J. D. McGeachy. 1993. « Aerodynamic performance of a transonic low aspect ratio turbine nozzle ». Journal of Turbomachinery. vol. 115 , nº 3. p. 400-408.
D. R. Whitehouse, S. H. Moustapha, S. A. Sjolander. 1993. « Effect of axial velocity ratio, turbulence intensity, incidence, and leading edge geometry on the midspan performance of a turbine cascade ». Canadian Aeronautics and Space Journal = Journal Aéronautique et Spatial du Canada. vol. 39 , nº 3. p. 150-156.
M. El-Fouly, H. Moustapha. 1990. « Application of 3-D flow analysis to the design of a high work transonic turbine ». Canadian Aeronautics and Space Journal = Journal Aéronautique et Spatial du Canada. vol. 36 , nº 2. p. 90-96.
S. H. Moustapha, S. C. Kacker, B. Tremblay. 1990. « An improved incidence losses prediction method for turbine airfoils ». Journal of Turbomachinery. vol. 112 , nº 2. p. 267-276.
U. W. Schaub, R. G. Williamson, J. P. Huot, S. H. Moustapha. 1990. « An experimental assessment of the influence of downstream conditions on the performance of a transonic turbine nozzle of high turning ». Journal of Turbomachinery. vol. 112 , nº 2. p. 286-293.
M. El-Fouly, H. Moustapha. 1990. « Application of 3-D flow analysis to the design of a high work transonic turbine ». Canadian Aeronautics and Space Journal = Journal Aéronautique et Spatial du Canada. vol. 36 , nº 2. p. 90-96.
S. H. Moustapha, S. C. Kacker, B. Tremblay. 1990. « An improved incidence losses prediction method for turbine airfoils ». Journal of Turbomachinery. vol. 112 , nº 2. p. 267-276.
U. W. Schaub, R. G. Williamson, J. P. Huot, S. H. Moustapha. 1990. « An experimental assessment of the influence of downstream conditions on the performance of a transonic turbine nozzle of high turning ». Journal of Turbomachinery. vol. 112 , nº 2. p. 286-293.
S. H. Moustapha, U. Okapuu, R. G. Williamson. 1987. « Influence of rotor blade aerodynamic loading on the performance of a highly loaded turbine stage ». Journal of Turbomachinery. vol. 109 , nº 2. p. 155-161.
S. H. Moustapha, U. Okapuu, R. G. Williamson. 1987. « Influence of rotor blade aerodynamic loading on the performance of a highly loaded turbine stage ». Journal of Turbomachinery. vol. 109 , nº 2. p. 155-161.
S. H. Moustapha, R. G. Williamson. 1986. « Effect of two endwall contours on the performance of an annular nozzle cascade ». AIAA Journal. vol. 24 , nº 9. p. 1524-1530.
R. G. Williamson, S. H. Moustapha. 1986. « Annular cascade testing of turbine nozzles at high exit mach numbers ». Journal of Fluids Engineering. vol. 108 , nº 3. p. 313-320.
R. G. Williamson, S. H. Moustapha, J. P. Huot. 1986. « The effect of a downstream rotor on the measured performance of a transonic turbine nozzle ». Journal of Turbomachinery. vol. 108 , nº 2. p. 269-274.
S. H. Moustapha, R. G. Williamson. 1986. « Effect of two endwall contours on the performance of an annular nozzle cascade ». AIAA Journal. vol. 24 , nº 9. p. 1524-1530.
R. G. Williamson, S. H. Moustapha. 1986. « Annular cascade testing of turbine nozzles at high exit mach numbers ». Journal of Fluids Engineering. vol. 108 , nº 3. p. 313-320.
R. G. Williamson, S. H. Moustapha, J. P. Huot. 1986. « The effect of a downstream rotor on the measured performance of a transonic turbine nozzle ». Journal of Turbomachinery. vol. 108 , nº 2. p. 269-274.
S. H. Moustapha, G. J. Paron, J. H. T. Wade. 1985. « Secondary flow in cascades of highly loaded turbine blades ». Journal of Engineering for Gas Turbines and Power. vol. 107 , nº 4. p. 1031-1038.
S. H. Moustapha, G. J. Paron, J. H. T. Wade. 1985. « Secondary flow in cascades of highly loaded turbine blades ». Journal of Engineering for Gas Turbines and Power. vol. 107 , nº 4. p. 1031-1038.
U. Okapuu, S. H. Moustapha. 1982. « Discussion: "Rotor tip leakage: Part II - Design optimization through viscous analysis and experiment” (Wadia, A. R., and Booth, T. C., 1982, ASME J. Eng. Power, 104, pp. 162–169) ». Journal of Engineering for Gas Turbines and Power. vol. 104 , nº 2. p. 522.
U. Okapuu, S. H. Moustapha. 1982. « Discussion: "Rotor tip leakage: Part II - Design optimization through viscous analysis and experiment” (Wadia, A. R., and Booth, T. C., 1982, ASME J. Eng. Power, 104, pp. 162–169) ». Journal of Engineering for Gas Turbines and Power. vol. 104 , nº 2. p. 522.