Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45©� sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶

Author:	Bingham, Gene J.
Additional Authors:	Braslow, Albert L.
Year:	1954
Document Type:	MAIN
SUDOC:	Y 3.N21/5:15/L54B18a
Series:	NACA research memorandum ;
Report Number:	L54B18a
Subjects:	Airplanes--Fuselage
	Airplanes--Wings, Swept-back--Handling characteristics
Link:	https://hdl.handle.net/2027/mdp.39015095100783