(1976). Experimental effects of fuselage camber on longitudinal aerodynamic characteristics of a series of wing-fuselage configurations at a Mach number of 1.41 / Samuel M. Dollyhigh, Odell A. Morris, and Mary S. Adams.
Chicago Style (17th ed.) CitationExperimental Effects of Fuselage Camber on Longitudinal Aerodynamic Characteristics of a Series of Wing-fuselage Configurations at a Mach Number of 1.41 / Samuel M. Dollyhigh, Odell A. Morris, and Mary S. Adams. 1976.
MLA (9th ed.) CitationExperimental Effects of Fuselage Camber on Longitudinal Aerodynamic Characteristics of a Series of Wing-fuselage Configurations at a Mach Number of 1.41 / Samuel M. Dollyhigh, Odell A. Morris, and Mary S. Adams. 1976.
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