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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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