Effects of Inlet Modification and Rocket-Rack Extension on the Longitudinal Trim and Low-Lift Drag of the Douglas F5D-1 Airplane as Obtained with a 0.125-Scale Rocket-Boosted Model Between Mach Numbers of 0.81 and 1.64: TED No. NACA AD 399

Author:	Hastings, Earl C., Jr.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-SL57D30
Link:	https://digital.library.unt.edu/ark:/67531/metadc64028/