Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tipssupersonic leading edges

Author:	Harmon, Sidney M
Year:	1950
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2156
Link:	https://digital.library.unt.edu/ark:/67531/metadc55498/