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Minimum Drag of Four Versions of a Swept-Wing Fighter Airplane Obtained From Flight Tests of Rocket-Boosted Models at Mach Numbers From 0.81 to 1.71
Author:
Hastings, Earl C., Jr.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56E25A
Link:
https://digital.library.unt.edu/ark:/67531/metadc53077/
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