Research Catalog

Parametric studies of shock wave/boundary layer interactions over 2D compression corners at Mach 6

Title
Parametric studies of shock wave/boundary layer interactions over 2D compression corners at Mach 6 / J.P. Vermeulen & G. Simeonides.
Author
Vermeulen, J. P.
Publication
Rhode Saint Genèse, Belgium : Von Karman Institute for Fluid Dynamics, [1992]

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StatusFormatAccessCall NumberItem Location
TextRequest in advance TL574.S4 V46 1992gOff-site

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Details

Additional Authors
Simeonides, G.
Description
xiii, 53 pages, 75 unnumbered pages : illustrations; 29 cm.
Series Statement
Technical note (Von Karman Institute for Fluid Dynamics) ; 181
Uniform Title
Technical note (Von Karman Institute for Fluid Dynamics) ; 181.
Alternative Title
Parametric studies of shock wave/boundary layer interactions over two-dimensional compression corners at Mach six.
Subject
  • Shock waves > Mathematical models
  • Turbulent boundary layer > Mathematical models
  • Laminar flow > Mathematical models
  • Aerodynamics, Hypersonic
  • Space vehicles > Atmospheric entry
  • Heat > Transmission
  • Thermography
  • Hypersonic planes > Design and construction
Note
  • "D/1992/0238/405"--P. [2] of cover.
  • "September 1992."
Bibliography (note)
  • Includes bibliographical references (p. 43-46).
OCLC
  • 27991195
  • ocm27991195
Owning Institutions
Columbia University Libraries