Airfoil profiles for minimum pressure drag at supersonic velocities: Application of shock-expansion theory, including consideration of hypersonic range

Author:	Chapman, Dean R.
Year:	1952
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2787
Link:	https://digital.library.unt.edu/ark:/67531/metadc56307/