Experimental effects of fuselage camber on longitudinal aerodynamic characteristics of a series of wing-fuselage configurations at a mach of 1.41 / Samuel M. Dollyhigh, Odell A. Morris, and Mary S. Adams ; Langley Research Center, Hampton, Va.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Dollyhigh, Samuel M.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Morris, Odell A., Adams, Mary S.
Format:	Government Document Book
Language:	English
Published:	Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976.
Series:	NASA technical memorandum ; X-3411.
Subjects:	Airplanes > Fuselage. Airplanes > Design and construction.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3411
NAS 1.15:3411	Available Place a Hold