Item Details

A Low Speed Wind Tunnel Investigation of Reynolds Number Effects on a 60-Deg. Swept Wing Configuration With Leading and Trailing Edge Flaps [microform]

Dhanvada M. Rao and Keith D. Hoffler
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1988]
Language
English
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:181684
Description
1 v.
Notes
Distributed to depository libraries in microfiche.
Reproduction Notes
Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 1 microfiche.
Series Statement
NASA contractor report ; 181684
NASA contractor report NASA CR-181684
Technical Details

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    a| A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps h| [microform] / c| Dhanvada M. Rao and Keith D. Hoffler.
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    a| Airplanes x| Wings x| Testing.
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