Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds / William P. Henderson ; Langley Research Center.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Henderson, William P.
Corporate Authors:	United States. National Aeronautics and Space Administration, Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976.
Series:	NASA technical note ; D-8361.
Subjects:	Airplanes > Wings, Swept-back.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-8361
NAS 1.14:D-8361	Available Place a Hold