Generalized area rules and integral theorems for hypersonic wing-bodies

DOI10.2514/3.7605zbMath0404.76051OpenAlexW2071989278MaRDI QIDQ4190337

Norman Malmuth

Publication date: 1978

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.7605

zbMATH Keywords

SupersonicSubsonicHigh-Acceleration MissilesHypersonic DeltaHypersonic TransportNonlinear Flow SolutionsParametric DependenciesScramjet VehiclesShock Waves-Capturing TechniquesShuttle Orbiter

Mathematics Subject Classification ID

Transonic flows (76H05) General aerodynamics and subsonic flows (76G25) Supersonic flows (76J20) Hypersonic flows (76K05)

Related Items (1)

Extremal problems of heat transfer to three-dimensional bodies at hypersonic speeds

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