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Theoretical investigation of the effects of configuration changes on the center-of-pressure shift of a body-wing-tail combination due to angle of attack and mach number at transonic speeds
Author:
Spahr, J Richard
Year:
1957
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3966
Link:
https://digital.library.unt.edu/ark:/67531/metadc56462/
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