Effect of yaw at supersonic speeds on theoretical aerodynamic coefficients of thin pointed wings with several types of trailing edge

Author:	Moeckel, W. E.
Year:	1948
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1549
Link:	https://digital.library.unt.edu/ark:/67531/metadc54825/