Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
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Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system

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Published by National Aeronautics and Space Administration, Glenn Research Center, Available from NASA Center for Aerospace Information in [Cleveland, Ohio], Hanover, MD .
Written in English

Subjects:

  • Air breathing boosters.,
  • Hypersonic speed.,
  • Computational fluid dynamics.,
  • Wind tunnel tests.,
  • Propulsion.,
  • Pressure distribution.

Book details:

Edition Notes

StatementJ.R. DeBonis and C.J. Trefny.
Series[NASA technical memorandum] -- NASA/TM-2001-210567., NASA technical memorandum -- 210567.
ContributionsTrefny, C. J., NASA Glenn Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL16028849M

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