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Effect of angle of attack and thickness on aerodynamic coefficients of a rigid wing oscillating at very low frequencies in two-dimensional supersonic flow
Author:
Malvestuto, Frank S., Jr.
Year:
1958
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-4069
Link:
https://digital.library.unt.edu/ark:/67531/metadc56851/
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