Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65̊ swept delta wing / by Jim A. Penland, Theodore R. Creel, Jr., and Floyd G. Howard.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Penland, Jim A.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Creel, Theodore R., Howard, Floyd G.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:	NASA technical note ; D-7633.
Subjects:	Hypersonic planes > Stability. Airplanes > Wings, Triangular.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-7633
NAS 1.14:D-7633	Available Place a Hold