Computation of inlet/forebody interaction flowfields is presented in the form of the view-graphs. The main objective was to develop 3-D Navier-Stokes capability which can be used to efficiently compute hypersonic, chemically reacting flowfields.
Computation of Inlet/Forebody Interaction Flowfields
1991
38 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Jet & Gas Turbine Engines , Fluid Mechanics , Computational fluid dynamics , Engine airframe integration , Flow distribution , Hypersonic flow , Inlet airframe configurations , Navier-stokes equation , Chemical reactions , Combustible flow , Computer programs , Computerized simulation , Euler equations of motion , Three dimensional flow
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