The accomplishments made in the following three tasks are described: (1) The first task was to study shock-wave boundary-layer interactions with bleed - this study is relevant to boundary-layer control in external and mixed-compression inlets of supersonic aircraft; (2) The second task was to test RAAKE, a code developed for computing turbulence quantities; and (3) The third task was to compute flow around the Ames ER-2 aircraft that has been retrofitted with containers over its wings and fuselage. The appendices include two reports submitted to AIAA for publication.
Numerical Study of Boundary-Layer in Aerodynamics
1997
52 pages
Report
Keine Angabe
Englisch
Aerodynamics , Boundary layer flow , Boundary layer control , Computational fluid dynamics , Computer programs , Flat plates , U-2 aircraft , Bleeding , Hole geometry(Mechanics) , Pressure gradients , Spacing , Turbulent flow , Supersonic flow , Computerized simulation , Fuselages , Wings , Oblique shock waves , Baldwin-lomax turbulence model , Shock wave interaction
Numerical Study of Boundary-Layer in Aerodynamics
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