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Liste des publications de "Germain, Patrick"Nombre de documents archivés : 19. Aitchison, Paul Archibald, Germain, Patrick David et Smith, Henry (inventeurs) 3 octobre 2006. « Normally open reverse flow flapper valve ». Pratt & Whitney Canada Corp. (titulaire(s)). Brevet américain US 7,114,519 B2. Albero, Jose, Dussault, Richard, Thompson, Robert G., Germain, Patrick, Sahm, Michael K. et Tremaine, Eric (inventeurs) 22 mars 2005. « Main propulsion engine system integrated with secondary power unit ». United Technologies Corporation (titulaire(s)). Brevet américain US 6,868,664 B2.
Brown, David A., Nadarajah, Siva, Yang, Hong, Castonguay, Patrice, Raiesi, Hassan, Sermeus, Kurt et Germain, Patrick.
2019.
« Quality-preserving linear elasticity mesh movement algorithm for multi-element unstructured meshes ».
AIAA Journal, vol. 57, nº 2.
pp. 521-531.
Brown, David A., Nadarajah, Sivakumaran, Hong, Yang, Castonguay, Patrice, Raiesi, Hassan, Sermeus, Kurt et Germain, Patrick.
2018.
« A linear elasticity mesh mover with adaptive mesh element stiffening for multi-element unstructured grids ».
In AIAA Aerospace Sciences Meeting (Kissimmee, FL, USA, Jan. 08-12, 2018)
Coll. « AIAA Paper », vol. AIAA 2018-0917.
American Institute of Aeronautics and Astronautics.
Germain, P. D. et Hornung, H. G..
1997.
« Transition on a slender cone in hypervelocity flow ».
Experiments in Fluids, vol. 22, nº 3.
pp. 183-190.
Germain, P., Cummings, E. et Hornung, H..
1993.
« Transition on a sharp cone at high enthalpy : New measurements in the shock tunnel T5 at GALCIT ».
In 31st Aerospace Sciences Meeting (Reno, NV, USA, Jan. 11-14, 1993)
AIAA.
Germain, P. et Hornung, H..
1995.
« The boundary layer on a sharp cone in high-enthalpy flow ».
In Shock Waves @ Marseille I : Hypersonics, Shock Tube & Shock Tunnel Flow (Marseille, France, July 26-30, 1993)
pp. 63-68.
Berlin, Heidelberg : Springer Berlin Heidelberg. Germain, Patrick. 1994. « The boundary layer on a sharp cone in high-enthalpy flow ». Thèse de doctorat. Los Angeles, Californie, California Institute of Technology
Germain, Patrick.
1990.
« Three samples of inviscid supersonic reacting nozzle flow calculation using SURF ».
Coll. « CaltechGALCITFM », vol. FM 90-2.
California Institute of Technology. Germain, Patrick et Bruno, Vittorio (inventeurs) 25 avril 2006. « Axisymmetric flap on gas turbine exhaust centerbody ». Pratt & Whitney Canada Corp. (titulaire(s)). Brevet américain US 7,032,387.
Hornung, H. G., Cummings, E. B., Germain, P., Sanderson, S. R., Sturtevant, B. et Wen, C. Y..
1994.
« Recent results from hypervelocity research in T5 ».
In AIAA 25th Plasmadynamics and Lasers Conference (Colorado Springs, CO, USA, June 20-23, 1994)
American Institute of Aeronautics and Astronautics Inc, AIAA.
Hornung, H.G., Adam, P., Germain, P., Fujii, K. et Rasheed, A..
2002.
« On transition and transition control in hypervelocity flow ».
In Proceedings of the Ninth Asian Congress of Fluid Mechanics (Isfahan, Iran, May 27-31, 2002)
Hornung, Hans, Wen, Chihyung et Germain, Patrick.
1994.
« Hypervelocity flow simulation ».
Applied Mechanics Reviews, vol. 47, nº 6S.
S14-S19.
Lei, Zhijun, Mahallati, Ali, Cunningham, Mark et Germain, Patrick.
2012.
« Effects of core flow swirl on the flow characteristics of a scalloped forced mixer ».
Journal of Engineering for Gas Turbines and Power, vol. 134, nº 11.
Lei, Zhijun, Mahallati, Ali, Cunningham, Mark et Germain, Patrick.
2010.
« Influence of inlet swirl on the aerodynamics of a model turbofan lobed mixer ».
In ASME 2010 International Mechanical Engineering Congress and Exposition (IMECE) (Vancouver, BC, Canada, Nov. 12-18, 2010)
pp. 807-819.
American Society of Mechanical Engineers (ASME). Marini, Remo, Germain, Patrick et Vrljes, Ljubisa (inventeurs) 12 juillet 2016. « Air cooler system for gas turbine engines ». Pratt & Whitney Canada Corp. (titulaire(s)). Brevet américain US 9,388,739 B2.
Meslioui, Sid-Ali, Cunningham, Mark et Germain, Patrick.
2007.
« Determination of CFD turbulence scales for lobed mixer jet noise prediction ».
In 2007 ASME Turbo Expo (Montreal, QC, Canada, May 14-17, 2007)
pp. 1541-1549.
American Society of Mechanical Engineers. Olver, Bryan, Ciampa, Alessandro, Marrano, Roberto, Trepanier, Richard, Lamarre, Sylvain, Bernard, Martin et Germain, Patrick (inventeurs) 4 janvier 2011. « Turbofan bypass duct air cooled fluid cooler installation ». Pratt and Whitney Canada Corp. (titulaire(s)). Brevet américain US 7,861,512 B2.
Tam, A., Robichaud, M. P., Tremblay, P., Habashi, W. G., Hohmeyer, M., Peeters, M. F., Guevremont, G. et Germain, P..
1998.
« A 3-D adaptive anisotropic method for external and internal flows ».
In 36th AIAA Aerospace Sciences Meeting and Exhibit (Reno, NV, USA, Jan. 12-15, 1998)
American Institute of Aeronautics and Astronautics Inc, AIAA. |