Angle-of-attack-supersonic performance of a configuration consisting of a ramp-type scoop inlet located either on top or bottom of a body of revolution

Author: Kremzier, Emil J.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E54C09
Link: https://digital.library.unt.edu/ark:/67531/metadc60314/

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