The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover /
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| Author / Creator: | Bousman, William G. (William Giles) |
|---|---|
| Imprint: | Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1990. |
| Description: | vii, 56 pages : illustrations ; 28 cm. |
| Language: | English |
| Series: | NASA technical paper ; 3002 AVSCOM technical report ; 89-A-002 NASA technical paper ; 3002. AVSCOM technical report ; 89-A-002. |
| Subject: | |
| Format: | E-Resource Microform U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/6508784 |
MARC
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| 100 | 1 | |a Bousman, William G. |q (William Giles) | |
| 245 | 1 | 4 | |a The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover / |c William G. Bousman. |
| 264 | 1 | |a Washington, D.C. : |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; |a [Springfield, Va.] : |b [For sale by the National Technical Information Service], |c 1990. | |
| 300 | |a vii, 56 pages : |b illustrations ; |c 28 cm. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a microform |b h |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/h | ||
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| 490 | 1 | |a NASA technical paper ; |v 3002 | |
| 490 | 1 | |a AVSCOM technical report ; |v 89-A-002 | |
| 500 | |a Prepared at Ames Research Center and the Aeroflightdynamics Directorate, U.S. Army Aviation Research and Technology Activity. | ||
| 504 | |a Includes bibliographical references : (page 56). | ||
| 538 | |a Available via Internet from the NASA Technical Report Server web site. Address as of 12/2/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900019187%5F1990019187.pdf ; current access is available via PURL. | ||
| 650 | 0 | |a Rotors (Helicopters) |x Stability. | |
| 650 | 0 | |a Rotors (Helicopters) |x Aerodynamics. |0 http://id.loc.gov/authorities/subjects/sh85115511 | |
| 650 | 0 | |a Aeroelasticity. |0 http://id.loc.gov/authorities/subjects/sh85001300 | |
| 650 | 7 | |a Coupling. |2 nasat | |
| 650 | 7 | |a Hovering. |2 nasat | |
| 650 | 7 | |a Hovering stability. |2 nasat | |
| 650 | 7 | |a Mathematical models. |2 nasat | |
| 650 | 7 | |a Rigid rotors. |2 nasat | |
| 650 | 7 | |a Rotary wings. |2 nasat | |
| 710 | 2 | |a Ames Research Center. |0 http://id.loc.gov/authorities/names/n79138699 |1 http://viaf.org/viaf/131341285 | |
| 710 | 1 | |a United States. |b Army Aviation Research and Technology Activity. |0 http://id.loc.gov/authorities/names/no90015738 |1 http://viaf.org/viaf/149204595 | |
| 830 | 0 | |a NASA technical paper ; |v 3002. | |
| 830 | 0 | |a AVSCOM technical report ; |v 89-A-002. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS65436 |y Government Publishing Office |
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/LPS65436 |z Government Publishing Office |g ebooks |i 12738936 | ||