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ElectronicResource GovDoc
Author Reed, Wilmer H.

Title An airfoil flutter model suspension system to accommodate large static transonic airloads [electronic resource] / Wilmer H. Reed, III.

Imprint Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
Connect to
Connect to https://permanent.fdlp.gov/gpo21276/19860004750-1986004750.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860004750.pdf

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:177998    ---  Available
Description 1 online resource (36 p.) : ill.
Series NASA contractor report ; 177998
NASA-CR-177998
NASA contractor report ; NASA CR-177998.
Note Title from title screen (viewed Apr. 10, 2012).
"October 1985."
Bibliography Includes bibliographical references (p. 18-19).
Funding Contract no. NAS1-17686 D-8402-3 505-63-21-02
Subject Airfoils.
Blowdown wind tunnels.
Flutter analysis.
Pressure distribution.
Static pressure.
Supercritical airfoils.
Transonic wind tunnels.
Two dimensional flow.
Added Author DEI-Tech, Inc.
Langley Research Center.
Other Form: Print version: Reed, Wilmer H. Airfoil flutter model suspension system to accommodate large static transonic airloads. (OCoLC)785222077
Microfiche: Reed, Wilmer H. Airfoil flutter model suspension system to accommodate large static transonic airloads. (OCoLC)466740867
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:177998

 
    
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