Theoretical calculation of the pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to the axis of wing symmetry

Author:	Margolis, Kenneth
Additional Authors:	Sherman, Windsor L.
Year:	1953
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2898
Link:	https://digital.library.unt.edu/ark:/67531/metadc57003/