Corrections for Lift, Drag, and Moment of an Airfoil in a Supersonic Tunnel Having a Given Static Pressure Gradient

Author: Ludloff, H. F.
Year: 1952
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2849
Link: https://digital.library.unt.edu/ark:/67531/metadc56509/

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