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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
Author:
Musial, Norman T
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E56K23
Link:
https://digital.library.unt.edu/ark:/67531/metadc63297/
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