Experimental Study and Analysis of Loading and Pressure Distributions on Delta Wings Due to Thickness and to Angle of Attack at Supersonic Speeds

Author: Boatright, William B.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56I14
Link: https://digital.library.unt.edu/ark:/67531/metadc63041/

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