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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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