Comparison of effect of a turbojet engine and three cold-flow configurations on the stability of a full-scale supersonicle inlet
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Comparison of effect of a turbojet engine and three cold-flow configurations on the stability of a full-scale supersonicle inlet, report, January 24, 1957; (https://digital.library.unt.edu/ark:/67531/metadc63297/: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.