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 ([NASA technical memorandum] ; NASA/TM-2001-210567)
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
原資料の出版事項: [Cleveland, Ohio] ; Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center : Available from NASA Center for Aerospace Information, [2001]