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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