Theoretical calculations of the effects of finite sideslip at supersonic speeds on the span loading and rolling moment for families of thin sweptback tapered wings at an angle of attack

Author: Sherman, Windsor L
Year: 1953
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3046
Link: https://digital.library.unt.edu/ark:/67531/metadc56736/

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