Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow

Author:	Chapman, Dean R.
Year:	1952
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1063, NACA-TN-2264
Link:	https://digital.library.unt.edu/ark:/67531/metadc60418/