Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of a double-cone axisymmetric inlet at Mach numbers from 3.0 to 2.0
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Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of a double-cone axisymmetric inlet at Mach numbers from 3.0 to 2.0, report, August 30, 1957; (digital.library.unt.edu/ark:/67531/metadc63620/: accessed April 27, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.