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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