Theoretical Analysis of Unswept Normal Shock Wave/Boundary Layer Interaction Control Using Streamwise Flaps
25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA
Aerodynamic measurement technology and ground testing conference ; AIAA Paper 2006-3198-2006-3354
2006-01-01
AIAA Paper 2006-3198-2006-3354
Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference
Aufsatz (Konferenz)
Englisch
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Investigation of Unswept Normal Shock Wave-Turbulent-Boundary-Layer Interaction Control
Online Contents | 2009
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