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Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges
Author:
Martin, John C
Additional Authors:
Margolis, Kenneth
Year:
1952
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-2699
Link:
https://digital.library.unt.edu/ark:/67531/metadc57267/
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