Communication to : Agard FDP WG 14 on : selections of test cases for CFD validation. To be published in A.R. 303SIGLEAvailable at INIST (FR), Document Supply Service, under shelf-number : 22419, issue : a.1993 n.161 / INIST-CNRS - Institut de l'Information Scientifique et TechniqueFRFranc
Approved for public release; distribution is unlimited. 20001018 006 The findings in this report are...
Communication to : 40th AIAA aerospace sciences meeting and exhibit, Reno, NV (USA), January 14-17, ...
Communication to : RTO AVT Symposium on vortex flow and high angle of attack, Loen (Norvege), May 07...
Abstract CFD examples at ADD are introduced to show their variety at its application in the course o...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
Tire de : Symposium AGARD/FDP 'Vortex flow aerodynamics', Scheveningen (Pays Bas), 1-4 octobre 1990A...
Communication to : AIAA/ICAS international air and space symposium and exhibition, Dayton (USA), 14-...
The use of computational fluid dynamics has risen in the past decade. With major advances in high pe...
The development of a wing/body/nacelle/pylon/horizontal-tail configuration for a common research mod...
© 2012 Jonathan Brian Da CostaThe simulation of missile systems plays an important role in the devel...
Communication to : Integrating CFD and experiments in aerodynamics, Glasgow (Royaume-Uni), 8-9 septe...
Tire de : AIAA 29th Aerospace Sciences Meeting, Reno NE (USA), January 7-10, 1991Available at INIST ...
Wind tunnel test results of an Anti-Tank Missile model with five different warheads are presented in...
This paper presents modification of the existing guided missile which was done by replacing the exis...
Communication to : 5th International symposium on liquid space propulsion - Long life combustion dev...
Approved for public release; distribution is unlimited. 20001018 006 The findings in this report are...
Communication to : 40th AIAA aerospace sciences meeting and exhibit, Reno, NV (USA), January 14-17, ...
Communication to : RTO AVT Symposium on vortex flow and high angle of attack, Loen (Norvege), May 07...
Abstract CFD examples at ADD are introduced to show their variety at its application in the course o...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
Tire de : Symposium AGARD/FDP 'Vortex flow aerodynamics', Scheveningen (Pays Bas), 1-4 octobre 1990A...
Communication to : AIAA/ICAS international air and space symposium and exhibition, Dayton (USA), 14-...
The use of computational fluid dynamics has risen in the past decade. With major advances in high pe...
The development of a wing/body/nacelle/pylon/horizontal-tail configuration for a common research mod...
© 2012 Jonathan Brian Da CostaThe simulation of missile systems plays an important role in the devel...
Communication to : Integrating CFD and experiments in aerodynamics, Glasgow (Royaume-Uni), 8-9 septe...
Tire de : AIAA 29th Aerospace Sciences Meeting, Reno NE (USA), January 7-10, 1991Available at INIST ...
Wind tunnel test results of an Anti-Tank Missile model with five different warheads are presented in...
This paper presents modification of the existing guided missile which was done by replacing the exis...
Communication to : 5th International symposium on liquid space propulsion - Long life combustion dev...
Approved for public release; distribution is unlimited. 20001018 006 The findings in this report are...
Communication to : 40th AIAA aerospace sciences meeting and exhibit, Reno, NV (USA), January 14-17, ...
Communication to : RTO AVT Symposium on vortex flow and high angle of attack, Loen (Norvege), May 07...