An approximate viscous shock layer technique for calculating chemically reacting hypersonic flows about blunt-nosed bodies
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An approximate viscous shock layer technique for calculating chemically reacting hypersonic flows about blunt-nosed bodies

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

Subjects:

  • Viscous flow.,
  • Aerodynamics, Hypersonic.

Book details:

Edition Notes

StatementF. McNeil Cheatwood and Fred R. DeJarnette.
SeriesNASA contractor report -- NASA CR-187617., NASA contractor report -- NASA CR-187617.
ContributionsDeJarnette, Fred R., Langley Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15377005M

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