Supersonic flow past a bent delta wing and its aerodynamic characteristics

DOI10.1023/A:1015151304222zbMath1046.76024OpenAlexW144036199MaRDI QIDQ1403555

R. Ya. Tugazakov, V. N. Golubkin, G. N. Dudin

Publication date: 3 September 2003

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1015151304222

zbMATH Keywords

Navier-Stokes equationslift-drag ratiohypersonic thin-shock-layer approximation

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20)

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