Investigation of flow variables over a series of rearward facing stepped flat plates at a nominal Mach number of 4.15.
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Investigation of flow variables over a series of rearward facing stepped flat plates at a nominal Mach number of 4.15.

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Published by Wright-Patterson Air Force Base in [Ohio] .
Written in English

Subjects:

  • Aerodynamics -- Flow.

Book details:

Edition Notes

SeriesTechnical documentary report ASD-TDR -- no. 63-131., Technical documentary report (Air Force Flight Dynamics Laboratory (U.S.)) -- no. 63-131.
ContributionsAir Force Flight Dynamics Laboratory (U.S.)
The Physical Object
Pagination73 p. :
Number of Pages73
ID Numbers
Open LibraryOL20922827M

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