State and development of flutter calculation / by A. Teichmann.
This report discusses the need for considering a wide variation in certain of the basic flutter parameters in conducting a flutter analysis. Conclusions are drawn stating that design charts or simple rules may be misleading. Due to inherent difficulties, dynamic model testing may also yield misleadi...
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| Main Author: | |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1951]
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| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 1297. |
| Subjects: |
MARC
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| 100 | 1 | |a Teichmann, A. | |
| 245 | 1 | 0 | |a State and development of flutter calculation / |c by A. Teichmann. |
| 260 | |a Washington, D.C. : |b National Advisory Commitee for Aeronautics, |c [1951] | ||
| 300 | |a 26 pages : |b illustrations ; |c 27 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 490 | 1 | |a Technical memorandum ; |v no. 1297. | |
| 500 | |a "March 1951." | ||
| 500 | |a NACA TM Number 1297. | ||
| 500 | |a Translated from Lilienthal-Gesellschaft fur Luftfahrtforschung, Berlin. Bericht 135, pp. 11-20, 1941, by the National Advisory Commitee for Aeronautics. | ||
| 520 | 3 | |a This report discusses the need for considering a wide variation in certain of the basic flutter parameters in conducting a flutter analysis. Conclusions are drawn stating that design charts or simple rules may be misleading. Due to inherent difficulties, dynamic model testing may also yield misleading results. The general flutter equations and various methods of solution are discussed. Of particular interest, curves are presented showing computational effort plotted against a number of degrees of freedom used in a flutter analysis. | |
| 650 | 0 | |a Flutter (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85049581. | |
| 650 | 0 | |a Airplanes |x Wings. |0 http://id.loc.gov/authorities/subjects/sh85002923. | |
| 650 | 0 | |a Ailerons. |0 http://id.loc.gov/authorities/subjects/sh85002551. | |
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| 650 | 7 | |a Airplanes |x Wings. |2 fast |0 (OCoLC)fst00803545. | |
| 650 | 7 | |a Flutter (Aerodynamics) |2 fast |0 (OCoLC)fst00928386. | |
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