Euler method characteristics, an F-14 fuselage geometry model and shock wave pattern predicted by Euler analysis, prediction of F-14 inlet pressure recovery levels, a fuselage induced inlet flow field comparison, avionic integration, and hypersonic vehicle inlet integration are among the topics covered. Information is given in viewgraph form.
Computational Simulations for Fighter and Hypersonic Vehicle Inlet-Forebody Interactions
1991
25 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Jet & Gas Turbine Engines , Spacecraft Trajectories & Flight Mechanics , Fluid Mechanics , Computational fluid dynamics , Flow distribution , Forebodies , Hypersonic inlets , Inlet airframe configurations , Inlet flow , Descriptive geometry , F-14 aircraft , Fuselages , Hypersonic vehicles , Avionics , Inlet pressure , Pressure recovery , Shock waves
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