Here, we present the Final Technical Report on AASERT Grant No. F49620-93-1-0476 Studies of Hypersonic Vehicle Flowfields, in support of AFOSR Grant F49620-93-0064 'Studies Of Hypersonic Boundary Layer Behavior'. The parent grant covered three interrelated research efforts: a study of the structure of hypersonic turbulent boundary layers and shock wave boundary layer interactions, a study of boundary layer transition at supersonic and hypersonic speeds, and the development and application of new optical techniques including filtered Rayleigh scattering and RELIEF to obtain multi-dimensional velocity and density data in the supersonic and hypersonic regimes.
Studies of Hypersonic Vehicle Flowfields
1996
7 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Aircraft , Turbulent boundary layer , Flow fields , Boundary layer transition , Hypersonic velocity , Hypersonic vehicles , Density , Optics , Shock waves , Vortices , Compressible flow , Rayleigh scattering , Filters , Mach number , Hypersonic characteristics , Supersonic characteristics , Laminar flow , Reynolds number , Boundary layer flow , Hypersonic flow , Ltvg(Low turbulence variable geometry)
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