Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-Edge Flap on a Delta Fin in Free Flight at Mach Numbers From 1.5 to 2.6

Author:	Chauvin, Leo T.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57B20
Link:	https://digital.library.unt.edu/ark:/67531/metadc63231/