Some Remarks on an Approximate Method of Estimating the Wave Drag Due to Thickness at Supersonic Speeds of Three-Dimensional Wings With Arbitrary Profile

Author:	Margolis, Kenneth
Year:	1952
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2619
Link:	https://digital.library.unt.edu/ark:/67531/metadc56267/