Rotating shake test and modal analysis of a model helicopter rotor blade /
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| Author / Creator: | Wilkie, W. Keats, author. |
|---|---|
| Imprint: | Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1997. |
| Description: | 1 online resource (15 pages.) : illustrations. |
| Language: | English |
| Series: | NASA technical memorandum ; 4760 NASA technical memorandum ; 4760. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10758181 |
MARC
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| 100 | 1 | |a Wilkie, W. Keats, |e author. | |
| 245 | 1 | 0 | |a Rotating shake test and modal analysis of a model helicopter rotor blade / |c W. Keats Wilkie, Paul H. Mirick, and Chester W. Langston. |
| 264 | 1 | |a Hampton, Virginia : |b National Aeronautics and Space Administration, Langley Research Center, |c June 1997. | |
| 300 | |a 1 online resource (15 pages.) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a NASA technical memorandum ; |v 4760 | |
| 500 | |a Title from title screen (viewed on Feb. 18, 2016). | ||
| 500 | |a "June 1997." | ||
| 500 | |a "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. | ||
| 500 | |a "ARL technical report 1389." | ||
| 504 | |a Includes bibliographical references (page 15). | ||
| 536 | |a Sponsored by the National Aeronautics and Space Administration |d WU 505-63-36-02 |d A5008 |d L-17352 | ||
| 650 | 7 | |a Rotary wings. |2 nasat | |
| 650 | 7 | |a Helicopters. |2 nasat | |
| 650 | 7 | |a Aeroelasticity. |2 nasat | |
| 650 | 7 | |a Hovering. |2 nasat | |
| 650 | 7 | |a Torsion. |2 nasat | |
| 650 | 7 | |a Aeroelasticity. |2 fast |0 http://id.worldcat.org/fast/fst00798235 | |
| 650 | 7 | |a Helicopters. |2 fast |0 http://id.worldcat.org/fast/fst00954597 | |
| 650 | 7 | |a Torsion. |2 fast |0 http://id.worldcat.org/fast/fst01152860 | |
| 700 | 1 | |a Mirick, Paul H., |e author. |0 http://id.loc.gov/authorities/names/no2014008488 |1 http://viaf.org/viaf/307453814 | |
| 700 | 1 | |a Langston, Chester W., |e author. | |
| 710 | 2 | |a Vehicle Technology Center (U.S. Army Research Laboratory) |0 http://id.loc.gov/authorities/names/no98068419 |1 http://viaf.org/viaf/144565110 | |
| 710 | 2 | |a Langley Research Center, |e issuing body. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration, |e sponsoring body. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
| 776 | 0 | 8 | |i Print version: |t Rotating shake test and modal analysis of a model helicopter rotor blade |w (OCoLC)437089421 |
| 776 | 0 | 8 | |i Microfiche version: |a Wilkie, W. Keats. |t Rotating shake test and modal analysis of a model helicopter rotor blade |w (OCoLC)41975252 |
| 830 | 0 | |a NASA technical memorandum ; |v 4760. | |
| 856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo65480 |y GPO Documents Without Shelves |
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