Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges

Author:	Harmon, Sidney M
Year:	1950
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2114
Link:	https://digital.library.unt.edu/ark:/67531/metadc55560/