Vibrational nonequilibrium stagnation shock layers at hypersonic speed and low Reynolds number

DOI10.1016/0017-9310(78)90102-3zbMath0393.76036OpenAlexW1987785449MaRDI QIDQ1252114

Barbara Schmitt-von Schubert

Publication date: 1978

Published in: International Journal of Heat and Mass Transfer (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0017-9310(78)90102-3

zbMATH Keywords

ContinuUm ApproachFree FlightHypersonic SpeedLow Reynolds NumberMerged Layer RegimePlane or Axisymmetric Blunt BodyStagnation StreamlineTranslational and Rotational TemperatureVelocity SlipVibrational Nonequilibrium Stagnation Shock LayersVibrational RelaxationVibrational TemperatureWind Tunnel

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

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Approximate boundary conditions for the flow of a mixture of reacting gases

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