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Author Wilbur, Matthew L., author.

Title Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads / Matthew L. Wilbur [and four others].

Publication Info. Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1998.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.15:1998-206281    ---  Available
Description 1 online resource (247 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA/TM ; 1998-206281
ARL-TR ; 1401
NASA technical memorandum ; 1998-206281.
ARL-TR (Aberdeen Proving Ground, Md.) ; 1401.
Note Title from title screen (viewed Aug. 3, 2016).
"January 1998."
"Performing organization: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center"--Report documentation page.
Bibliography Includes bibliographical references (page 5).
Type Of Report Technical memorandum.
Funding Sponsored by the National Aeronautics and Space Administration and U.S. Army Research Laboratory WU 505-63-36-02 PR A5008 L-17353
Subject Helicopters -- Vibration.
Structural dynamics.
Helicopters -- Vibration. (OCoLC)fst00954668
Structural dynamics. (OCoLC)fst01135648
Helicopters.
Rotary wing aircraft.
Loads (forces)
Rotor dynamics.
Wind tunnel tests.
Genre/Form Online resources.
Electronic books.
Electronic government information.
Added Author Langley Research Center, issuing body.
Vehicle Technology Center (U.S. Army Research Laboratory), issuing body.
Other Form: Print version: Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads (OCoLC)38329944
Gpo Item No. 0830-H-15 (online)
Sudoc No. NAS 1.15:1998-206281

 
    
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