Solutions for Three-Dimensional Over- or Underexpanded Exhaust Plumes

DOI10.2514/3.51179zbMath0496.76037OpenAlexW1620811601MaRDI QIDQ3960338

M. J. Werle, Veer N. Vatsa, Orson L. Anderson, G. B. Hankins

Publication date: 1982

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.51179

zbMATH Keywords

streamline curvaturethree- dimensionalapproximate inviscid flow intrinsic coordinate systemexhaust plumeshigh-aspect-ratio slot jet flowslinearized perturbation potentialsslightly under- or overexpanded supersonic jet

Mathematics Subject Classification ID

Supersonic flows (76J20) Wakes and jets (76D25) Basic methods in fluid mechanics (76M99)

Related Items (1)

Numerical calculations of supersonic underexpanded jets in a cocurrent flow with the use of parabolized Navier-Stokes equations

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