An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds

Author:	Czarnecki, K. R.
Year:	1950
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2211
Link:	https://digital.library.unt.edu/ark:/67531/metadc55601/