My Account Log in

2 options

Rotating shake test and modal analysis of a model helicopter rotor blade / W. Keats Wilkie, Paul H. Mirick, and Chester W. Langston.

Online

Available online

View online

U.S. Government Documents Available online

View online
Format:
Book
Government document
Author/Creator:
Wilkie, W. Keats, author.
Mirick, Paul H., author.
Langston, Chester W., author.
Contributor:
Vehicle Technology Center (U.S. Army Research Laboratory)
Langley Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Series:
NASA technical memorandum ; 4760.
NASA technical memorandum ; 4760
Language:
English
Subjects (All):
Helicopters.
Aeroelasticity.
Torsion.
helicopters.
torsional stress.
Physical Description:
1 online resource (15 pages.) : illustrations.
Place of Publication:
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1997.
Notes:
Title from title screen (viewed on Feb. 18, 2016).
"June 1997."
"Performing organizations: NASA Langley Research Center, Hampton, VA [and] Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton, VA"--Report documentation page.
Includes bibliographical references (page 15).
"ARL technical report 1389."
Other Format:
Print version: Rotating shake test and modal analysis of a model helicopter rotor blade
Microfiche version: Wilkie, W. Keats. Rotating shake test and modal analysis of a model helicopter rotor blade
OCLC:
939619632

The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.

Find

Home Release notes

My Account

Shelf Request an item Bookmarks Fines and fees Settings

Guides

Using the Find catalog Using Articles+ Using your account