Pressure Distribution and Aerodynamic Coefficients Associated With Heat Addition to Supersonic Air Stream Adjacent to Two-Dimensional Supersonic Wing

Author:	Pinkel, I. Irving
Additional Authors:	Serafini, John S.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E51K26
Link:	https://digital.library.unt.edu/ark:/67531/metadc59929/