Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny.
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| Format: | Government Document Microfilm Book |
| Language: | English |
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[Cleveland, Ohio] : Hanover, MD :
National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information,
[2001]
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| Series: | NASA technical memorandum ;
210567. |
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| Item Description: | Shipping list number: 2002-0157-M. |
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| Physical Description: | 1 volume. |
| Reproduction Note: | Microfiche. |