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Improvement of forebody/inlet integration for hypersonic vehicle
Authors:NC Bissinger  NA Blagoveshchensky  AA Gubanov  VN Gusev  VP Starukhin  NV Voevodenko  SM Zadonsky
Institution:aDaimler Benz Aerospace AG, MT633, 81663 München, Germany;bCentral Aerohydrodynamic Institute, TsAGI, 140160 Zhukovsky, Moscow region, Russia
Abstract:Results of a numerical (CFD) study of the influence of the forebody shape on local flow parameters at a bottom-mounted inlet entrance are presented. The free-stream Mach number is assumed to be 3.5–7.0. Some recommendations on forebody shape optimization are provided. Main characteristics of the air inlet are evaluated.
Keywords:hypersonic inlet characteristics  forebody-inlet integration  hypersonic small-disturbance theory  Godunov's methodEinlaufcharakteristiken im Hyperschall  Vorkö  rper-Einlauf Integration  Theorie kleiner Stö  rungen im Hyperschall  Godunov's Methode
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