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Influence of boundary layer on unsteady aerodynamic characteristics of blunt cones in a supersonic flow

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Publication:761304
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DOI10.1007/BF01090553zbMath0555.76044OpenAlexW1975348945MaRDI QIDQ761304

V. A. Platonov, Yu. M. Lipnitskij, A. N. Pokrovskij, V. N. Sirenko, V. N. Shmanenkov

Publication date: 1983

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

Full work available at URL: https://doi.org/10.1007/bf01090553


zbMATH Keywords

supersonic gas streamlaminar and turbulent flow regimeslinear theory of bodies of finite thicknessunsteady aerodynamic characteristics of blunt coneszero angle of attack


Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20)





Cites Work

  • Influence of blowing on the characteristics of the nonstationary boundary layer on an oscillating wedge in a supersonic stream
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