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Liste des publications de "Moustapha, Hany"Nombre de documents archivés : 67.
Akel, Iyad, Habashi, Wagdi G. et Moustapha, Hany S..
2002.
« Toward CFD-based correlations for single-stage high-pressure transonic turbine stage ».
International Journal of Rotating Machinery, vol. 8, nº 5.
pp. 337-352.
Andronenko, Sergey, Stiharu, Ion, Packirisamy, Muthukuruman, Moustapha, Hany et Dionne, Patrice.
2005.
« The use of microelectromechanical systems for surge detection in gas turbine engines ».
In Proceedings - 2005 International Conference on MEMS, NANO and Smart Systems (ICMENS) (Banff, AB, Canada, July 24-27, 2006)
pp. 355-358.
Institute of Electrical and Electronics Engineers Computer Society.
Badger, M., Julien, A., LeBlanc, A. D., Moustapha, S. H., Prabhu, A. et Smailys, A. A..
1994.
« The PT6 engine: 30 years of gas turbine technology evolution ».
Journal of Engineering for Gas Turbines and Power, vol. 116, nº 2.
pp. 322-330.
Badger, M., Julien, A., LeBlanc, A. D., Moustapha, S. H., Prabhu, A. et Smailys, A. A..
1993.
« The PT6 engine: 30 years of gas turbine technology evolution ».
In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993 (Cincinnati, OH, USA, May 24-27, 1993)
ASME.
Banner, M. W., Sjolander, S. A. et Moustapha, S. H..
2003.
« The influence of leading-edge geometry on secondary losses in a turbine cascade at the design incidence ».
In ASME Turbo Expo 2003 (Atlanta, GA, USA, June 16-19, 2003)
pp. 147-161.
ASME.
Benner, M. W., Sjolander, S. A. et Moustapha, S. H..
2005.
« An empirical prediction method for secondary losses in turbines: Part I - A new loss breakdown scheme and penetration depth correlation ».
In ASME Turbo Expo 2005: Power for Land, Sea, and Air (Reno, NV, USA, June 06-09, 2005)
Coll. « Proceedings of the ASME Turbo Expo »
pp. 625-635.
ASME.
Benner, M. W., Sjolander, S. A. et Moustapha, S. H..
2005.
« An empirical prediction method for secondary losses in turbines: Part II - A new secondary loss correlation ».
In ASME Turbo Expo 2005: Power for Land, Sea, and Air (Reno, NV, USA, June 06-09, 2005)
Coll. « Proceedings of the ASME Turbo Expo »
pp. 637-649.
ASME.
Benner, M. W., Sjolander, S. A. et Moustapha, S. H..
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.
pp. 193-200.
Benner, M. W., Sjolander, S. A. et Moustapha, S. H..
1995.
« Influence of leading-edge geometry on profile losses in turbines at off-design incidence: Experimental results and an improved correlation ».
In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition, GT 1995 (Houston, TX, USA, June 05-08, 1995)
Coll. « Proceedings of the ASME Turbo Expo »
ASME.
Benner, M. W., Sjolander, S. A. et Moustapha, S. H..
2004.
« Measurements of secondary flows downstream of a turbine cascade at off-design incidence ».
In Proceedings of the ASME Turbo Expo 2004 (Vienna, Austria, June 14-17, 2004)
pp. 1299-1311.
ASME.
Benner, M. W., Sjolander, S. A. et Moustapha, S. H..
1997.
« Measurements of secondary flows in a turbine cascade at off-design incidence ».
In ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition (Orlando, FL, USA, June 02-05, 1997)
Coll. « Proceedings of the ASME Turbo Expo »
Benner, M. W., Sjolander, S. A. et Moustapha, S. H..
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.
pp. 277-287.
Benner, Michael W., Sjolander, S. A. et Moustapha, S. H..
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.
pp. 273-280.
Benner, Michael W., Sjolander, S. A. et Moustapha, S. H..
2006.
« An empirical prediction method for secondary losses in turbines - Part II: A new secondary loss correlation ».
Journal of Turbomachinery, vol. 128, nº 2.
pp. 281-291.
Blondin, Benoit, Lagloire, François, Moustapha, Hany et Ouellet, Yannick.
2013.
« Single platform integration enviroment for turbine rotor design and analysis ».
In XXI International Symposium on Air Breathing Engines (ISABE) (Busan, Korea, Sept. 09-13, 2013)
pp. 1148-1156.
AIAA.
Doran, Pascal, Vlasic, Ed, Guevremont, Grant et Moustapha, Hany.
2018.
« Gas-path optimization using turbine aerodynamics meanline and design exploration ».
In Proceedings of GPPS Society Forum 18 (Montréal, QC, Canada, May 07-09, 2018)
Global Power and Propulsion Society.
El Shammaa, S. A., Moustapha, S. H. et Wade, J. H. T..
1984.
« Secondary flow in cascades of high turning angle turbine blades ».
In First Parsons International Turbine Conference (Dublin, Ireland, June 28-29, 1984)
pp. 93-104.
Dublin, Ireland : Parsons Press.
El-Fouly, M. et Moustapha, H..
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.
pp. 90-96.
Girgis, S., Vlasic, E., Lavoie, J. P. et Moustapha, S. H..
2002.
« The effect of secondary air injection on the performance of a transonic turbine stage ».
In ASME Turbo Expo 2002: Power for Land, Sea, and Air (Amsterdam, The Netherlands, June 03-06, 2002)
pp. 147-157.
Habashi, W. G., Robichaud, M. P., Moustapha, S. H., Guèvremont, G. J. et Peeters, M. F..
1999.
« A practical and effective approach to cfd education, through a university-industry 1technology exchange perspective ».
In 37th Aerospace Sciences Meeting and Exhibit (Reno, NV, USA, Jan. 11-14, 1999)
AIAA.
Ibrahem, Ibrahem M. A., Akhrif, Ouassima, Moustapha, Hany et Staniszewski, Martin.
2020.
« An ensemble of recurrent neural networks for real time performance modelling of three-spool aero-derivative gas turbine engine ».
In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition (En ligne, Sept. 21-25, 2020)
ASME.
Ibrahem, Ibrahem M. A., Akhrif, Ouassima, Moustapha, Hany et Staniszewski, Martin.
2019.
« Neural networks modelling of aero-derivative gas turbine engine: a comparison study ».
In Proceedings of the 16th International Conference on Informatics in Control, Automation and Robotics (ICINCO) (Prague, Czech Republic, July 29-31, 2019)
pp. 738-745.
SciTePress.
Ibrahem, Ibrahem M. A., Akhrif, Ouassima, Moustapha, Hany et Staniszewski, Martin.
2021.
« Nonlinear generalized predictive controller based on ensemble of NARX models for industrial gas turbine engine ».
Energy, vol. 230.
Ibrahem, Ibrahem M. A, Akhrif, Ouassima, Moustapha, Hany et Staniszewski, Martin.
2020.
« Real time modeling and Hardware in the loop simulation of an aero-derivative gas turbine engine ».
In Proceedings of Global Power and Propulsion Society (En ligne, Sept. 07-09, 2020)
Siemens Energy Canada Limited.
Ibrahem, Ibrahem Mohamed, Akhrif, Ouassima, Moustapha, Hany et Staniszewski, Martin.
2021.
« An ensemble of recurrent neural networks for real time performance modelling of three-spool aero-derivative gas turbine engine ».
Journal of Engineering for Gas Turbines and Power, vol. 143, nº 10.
Jouini, D. B. M., Sjolander, S. A. et Moustapha, S. H..
2001.
« Aerodynamic performance of a transonic turbine cascade at off-design conditions ».
Journal of Turbomachinery, vol. 123, nº 3.
pp. 510-518.
Jouini, D. B. M., Sjolander, S. A. et Moustapha, S. H..
2000.
« Aerodynamic performance of a transonic turbine cascade at off-design conditions ».
In ASME Turbo Expo 2000: Power for Land, Sea, and Air (Munich, Germany, May 08-11, 2000)
Coll. « Proceedings of the ASME Turbo Expo »
ASME.
Jouini, D. B. M., Sjolander, S. A. et Moustapha, S. H..
2002.
« Midspan flow-field measurements for two transonic linear turbine cascades at off-design conditions ».
Journal of Turbomachinery, vol. 124, nº 2.
pp. 176-186.
Jouini, D. B. M., Sjolander, S. A. et Moustapha, S. H..
2001.
« Midspan flow-field measurements for two transonic linear turbine cascades at off-design conditions ».
In ASME Turbo Expo 2001: Power for Land, Sea, and Air (New Orleans, LA, USA, June 4-7, 2001)
Coll. « Proceedings of the ASME Turbo Expo »
American Society of Mechanical Engineers (ASME).
Lagloire, François, Ouellet, Yannick, Blondin, Benoit, Garnier, François et Moustapha, Hany.
2014.
« Single platform integration environment for turbine rotor design and analysis ».
Journal of Energy and Power Engineering, vol. 8, nº 9.
pp. 1590-1598.
Mesbah, Nacim, Seifert, Sandy, Chatelois, Bruno, Garnier, François et Moustapha, Hany.
2014.
« Parameterization modeling of a gas turbine coverplate ».
Journal of Energy and Power Engineering, vol. 9, nº 8.
pp. 1378-1385.
Moradi, Niloofar, Vlasic, Edward et Moustapha, Hany.
2015.
« Rapid airfoil design for uncooled high pressure turbine blades ».
In ASME Turbo Expo 2015: Turbine Technical Conference and Exposition (Montreal, QC, Canada, June 15-19, 2015)
American Society of Mechanical Engineers (ASME).
Moret, Maxime, Delecourt, Alexandre, Moustapha, Hany, Abenhaim, Acher-Igal et Garnier, Francois.
2017.
« Automated thermal and stress preliminary analyses applied to a turbine rotor ».
Aerospace Science and Technology, vol. 63.
pp. 123-131.
Moret, Maxime, Delecourt, Alexandre, Moustapha, Hany, Garnier, François et Abenhaim, Acher-Igal.
2016.
« Automated thermal and stress preliminary analyses applied to a turbine rotor ».
In ASME Turbo Expo : Turbomachinery Technical Conference and Exposition (Seoul, South Korea, June 13-17, 2016)
ASME International.
Moret, Maxime, Garnier, François, Phutthavong, Patricia et Moustapha, Hany.
2018.
« Automation of a turbine tip clearance preliminary calculation process ».
In Proceedings of GPPS Society Forum 18 (Montréal, QC, Canada, May 07-09, 2018)
Global Power and Propulsion Society.
Moret, Maxime, Moustapha, Hany, Garnier, François et Abenhaim, Acher-Igal.
2015.
« Automatic thermal and stress preliminary analyses applied to a turbine rotor ».
In 62nd CASI Aeronautics Conference and AGM 3rd GARDN (Montreal, QC, Canada, May 19-21, 2015)
CASI.
Moustapha, Hany.
2003.
« Future technology challenges for small gas turbines ».
In AIAA International Air and Space Symposium and Exposition: The Next 100 Years (Dayton, OH, 2003, July 14-17, 2003)
Coll. « AIAA paper », vol. AIAA 2003-2559.
AIAA.
Moustapha, S. H., Carscallen, W. E. et McGeachy, J. D..
1993.
« Aerodynamic performance of a transonic low aspect ratio turbine nozzle ».
Journal of Turbomachinery, vol. 115, nº 3.
pp. 400-408.
Moustapha, S. H., Carscallen, W. E. et McGeachy, J. D..
1992.
« Aerodynamic performance of a transonic low aspect ratio turbine nozzle ».
In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992 (Cologne, Germany, June 01-04, 1992)
ASME.
Moustapha, S. H., Kacker, S. C. et Tremblay, B..
1990.
« An improved incidence losses prediction method for turbine airfoils ».
Journal of Turbomachinery, vol. 112, nº 2.
pp. 267-276.
Moustapha, S. H., Kacker, S. C. et Tremblay, B..
1989.
« An improved incidence losses prediction method for turbine airfoils ».
In ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition (Toronto, ON, Canada, June 04-08, 1989)
Coll. « Proceedings of the ASME Turbo Expo »
ASME.
Moustapha, S. H., Okapuu, U. et Williamson, R. G..
1987.
« Influence of rotor blade aerodynamic loading on the performance of a highly loaded turbine stage ».
Journal of Turbomachinery, vol. 109, nº 2.
pp. 155-161.
Moustapha, S. H., Paron, G. J. et Wade, J. H. T..
1985.
« Secondary flow in cascades of highly loaded turbine blades ».
In 30th International Gas Turbine Conference and Exhibit (Houston, TX, USA
American Society of Mechanical Engineers.
Moustapha, S. H., Paron, G. J. et Wade, J. H. T..
1985.
« Secondary flow in cascades of highly loaded turbine blades ».
Journal of Engineering for Gas Turbines and Power, vol. 107, nº 4.
pp. 1031-1038.
Moustapha, S. H. et Williamson, R. G..
1986.
« Effect of two endwall contours on the performance of an annular nozzle cascade ».
AIAA Journal, vol. 24, nº 9.
pp. 1524-1530.
Moustapha, S. H. et Williamson, R. G..
1985.
« Investigation of the effect of two endwall contours on the performance of an annular nozzle cascade ».
In 21st Joint Propulsion Conference (Monterey, CA, USA, July 08-11, 1985)
AIAA.
Okapuu, U. et Moustapha, S. H..
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.
Ouellet, Y., Roy, F., Moustapha, H. et Garnier, F..
2013.
« Preliminary design of axial turbine disc for aicraft engines ».
In CASI 60th aeronautic conference (Toronto, ON, Canada, Apr. 30-May 02, 2013)
CASI.
Ouellet, Yannick, Garnier, François, Roy, François et Moustapha, Hany.
2014.
« A Preliminary Design System for Turbine Discs ».
In ASME Turbo Expo 2014: Turbine Technical Conference and Exposition (Düsseldorf, Germany, June 16–20, 2014)
ASME.
Ouellet, Yannick, Savaria, Christian, Roy, François, Moustapha, Hany et Garnier, François.
2019.
« A Preliminary design system for turbine discs ».
International Journal of Turbo and Jet Engines, vol. 36, nº 3.
pp. 329-338.
Raya, Maroua, Aidibe, Ali, Nadeau, Sylvie, Hof, Lucas et Moustapha, Hany.
2023.
« Livre blanc Réseau SDG Innovation: Au delà de l’industrie 4.0/5.0 : Vers une société Smart Digital Green ».
. 60 p.
Rodger, P., Sjolander, S. A. et Moustapha, S. H..
1992.
« Establishing two-dimensional flow in a large-scale planar turbine cascade ».
In AIAA/ASME/SAE/ASEE 28th Joint Propulsion Conference and Exhibit (Nashville, TN, USA, July 6-8, 1992)
AIAA.
Savaria, C., Phutthavong, P., Moustapha, H. et Garnier, F..
2018.
« Preliminary design for turbine housing and shroud segments ».
Aeronautical Journal, vol. 122, nº 1248.
pp. 260-282.
Savaria, Christian, Garnier, François, Moustapha, Hany et Phutthavong, Patricia.
2016.
« New correlations for high-pressure turbine housing and shroud segments ».
In ASME Turbo Expo : Turbomachinery Technical Conference and Exposition (Seoul, South Korea, June 13-17, 2016)
ASME International.
Schaub, U. W., Williamson, R. G., Huot, J. P. et Moustapha, S. H..
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.
pp. 286-293.
Schaub, U. W., Williamson, R. G., Huot, J. P. et Moustapha, S. H..
1989.
« An experimental assessment of the influence of downstream conditions on the performance of a transonic turbine nozzle of high turning ».
In ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition (Toronto, ON, Canada, June 04-08, 1989)
Coll. « Proceedings of the ASME Turbo Expo »
ASME.
Tremblay, B., Sjolander, S. A. et Moustapha, S. H..
1990.
« Off-Design performance of a linear cascade of turbine blades ».
In ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition (Brussels, Belgium, June 11–14, 1990)
Coll. « Proceedings of the ASME Turbo Expo »
ASME.
Twahir, Abdulhalim, Attia, Magdy, Roy, Franois et Moustapha, Hany.
2014.
« Preliminary design and analysis tool for aeroengine turbine fixings ».
In ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) (Montreal, QC, Canada, Nov. 14-20, 2014)
American Society of Mechanical Engineers (ASME).
Twahir, Abdulhalim, Moustapha, Hany, Doré, Sylvie et Roy, François.
2017.
« A framework for an integrated turbine rotor design system ».
In Global Power and Propulsion Forum : Proceedings (Zurich, Switzerland, Jan. 16-18, 2017)
Global Power & Propulsion Society.
Vlasic, E. P., Girgis, S. et Moustapha, S. H..
1996.
« The design and performance of a high work research turbine ».
Journal of Turbomachinery, vol. 118, nº 4.
pp. 792-799.
Vlasic, E. P., Girgis, S. et Moustapha, S. H..
1995.
« The design and performance of a high work research turbine ».
In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition (Houston, TX, USA, June 05-08, 1995)
Coll. « Proceedings of the ASME Turbo Expo »
Whitehouse, D. R., Moustapha, S. H. et Sjolander, S. A..
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.
pp. 150-156.
Williamson, R. G. et Moustapha, S. H..
1986.
« Annular cascade testing of turbine nozzles at high exit mach numbers ».
Journal of Fluids Engineering, vol. 108, nº 3.
pp. 313-320.
Williamson, R. G. et Moustapha, S. H..
1985.
« Three-dimensional cascade testing of turbine nozzles at high exit mach numbers ».
In 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)
pp. 45-54.
ASME.
Williamson, R. G., Moustapha, S. H. et Huot, J. P..
1986.
« The effect of a downstream rotor on the measured performance of a transonic turbine nozzle ».
Journal of Turbomachinery, vol. 108, nº 2.
pp. 269-274.
Woinowsky-Krieger, M., Lavoie, J. P., Vlasic, E. P. et Moustapha, S. H..
1998.
« Off-design performance of a single stage transonic turbine ».
In ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition (Stockholm, Sweden, June 02-05, 1998)
Coll. « Proceedings of the ASME Turbo Expo »
ASME.
Woinowsky-Krieger, M., Lavoie, J. P., Vlasic, E. P. et Moustapha, S. H..
1999.
« Off-design performance of a single-stage transonic turbine ».
Journal of Turbomachinery, vol. 121, nº 2.
pp. 177-183. |