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- W863668968 abstract "The effects of fuselage cross sections and structural members on the performance of hypersonic cruise aircraft are evaluated. Representative fuselage/tank area structure was analyzed for strength, stability, fatigue and fracture mechanics. Various thermodynamic and structural tradeoffs were conducted to refine the conceptual designs with the primary objective of minimizing weight and maximizing aircraft range." @default.
- W863668968 created "2016-06-24" @default.
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- W863668968 date "1975-01-01" @default.
- W863668968 modified "2023-09-26" @default.
- W863668968 title "A fuselage/tank structure study for actively cooled hypersonic cruise vehicles: Aircraft design evaluation" @default.
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- W863668968 hasPublicationYear "1975" @default.
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