Contributions

  • Saunders, J. D. - Contributor
  • United States. National Aeronautics and Space Administration. - Contributor

Publication

1995 - National Aeronautics and Space Administration, Washington, DC, District of Columbia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

Alternate Titles

  • 3D Navier Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet.

Subjects

Topics

Shock wavesEngine inletsLeading edgesInternal flowBoundary layersTurbulence modelsFlow distribution

Series Statement

  • NASA technical memorandum -- 107123.

Other Editions

  • 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inletMicroformNational Aeronautics and Space Administration1995-01-01

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