Influence of temperature factor on the aerodynamic characteristics of a circular cylinder in a supersonic perfect gas flow
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Publication:1815139
DOI10.1007/BF02230779zbMath0864.76042OpenAlexW1990850629MaRDI QIDQ1815139
V. A. Bashkin, M. V. Egorova, I. V. Egorov
Publication date: 7 November 1996
Published in: Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf02230779
Navier-Stokes equationstemperature factorisothermal surfacestermally insulated surfaceszero yaw angle
Related Items (2)
Calculation of the supersonic perfect gas flow in an hypersonic air-intake ⋮ Initiation and development of separated flow behind a circular cylinder in a supersonic stream
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