Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack

DOI10.1016/S0045-7825(96)01203-0zbMATH Open0923.76189OpenAlexW2093265126MaRDI QIDQ1388008

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Publication date: 24 September 1998

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7825(96)01203-0

Mathematics Subject Classification ID

Transonic flows (76H05) General aerodynamics and subsonic flows (76G25) Conformal mappings of special domains (30C20) Supersonic flows (76J20)

Cites Work

• Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack

Related Items (2)

Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack ⋮ Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft

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