Terminal-shock and restart control of a Mach 2.5, axisymmetric, mixed compression inlet with 40 percent internal contraction /
by Robert J. Baumbick, Robert E. Wallhagen, and Robert C. Seidel.
APA Citation
Baumbick, R. J., Seidel, R. C., Wallhagen, R. E., Lewis Research Center. (1974). Terminal-shock and restart control of a Mach 2.5, axisymmetric, mixed compression inlet with 40 percent internal contraction. Washington, D.C.: National Aeronautics and Space Administration .
MLA Citation
Baumbick, Robert J, Robert C Seidel, Robert E Wallhagen, and Lewis Research Center. Terminal-shock And Restart Control of a Mach 2.5, Axisymmetric, Mixed Compression Inlet With 40 Percent Internal Contraction. Washington, D.C.: National Aeronautics and Space Administration , 1974.
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