Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6 / by Robert J. Mack.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Mack, Robert J.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
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-7753.
Subjects:	Airplanes > Wings > Testing. Aerodynamics, Supersonic. Leading edges (Aerodynamics) Lift (Aerodynamics) Camber (Aerofoils)

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-7753
NAS 1.14:D-7753	Available Place a Hold