Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 /

Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 /

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Bibliographic Details
Author / Creator:Landrum, Emma Jean, author.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, October 1968.
Description:1 online resource (20 pages) : illustrations.
Language:English
Series:NASA technical note ; TN D-4796
NASA technical note ; D-4796.
Subject:
Aerodynamics, Supersonic.
Camber (Aerofoils)
Mach number.
Reynolds number.
Aerodynamics, Supersonic.
Camber (Aerofoils)
Mach number.
Reynolds number.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12674925
Hidden Bibliographic Details
Other authors / contributors:Shrout, Barrett L., author.
United States. National Aeronautics and Space Administration, issuing body.
Langley Research Center.
Notes:"October 1968."
Includes bibliographical references (page 7).
Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 17, 2020).
Other form:Print version: Landrum, Emma Jean Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03
GPO item no.:0830-H-13 (online)
Govt.docs classification:NAS 1.14:D-4796

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