Influence of boundary layer on unsteady aerodynamic characteristics of blunt cones in a supersonic flow
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
supersonic gas streamlaminar and turbulent flow regimeslinear theory of bodies of finite thicknessunsteady aerodynamic characteristics of blunt coneszero angle of attack
General aerodynamics and subsonic flows (76G25) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20)
Cites Work
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