| タイトル | Development, Analysis and Testing of the High Speed Research Flexible Semispan Model |
| 本文（外部サイト） | http://hdl.handle.net/2060/19990094230 |
| 著者（英） | Spain, Charles V.; Vogler, William A.; Schuster, David M.; Rausch, Russ D.; Stockwell, Alan E.; Hamouda, M-Nabil; Turnock, David L. |
| 著者所属（英） | Lockheed Martin Engineering and Science Services |
| 発行日 | 1999-09-01 |
| 言語 | eng |
| 内容記述 | This report presents the work performed by Lockheed Martin Engineering and Sciences (LMES) in support of the High Speed Research (HSR) Flexible Semispan Model (FSM) wind-tunnel test. The test was conducted in order to assess the aerodynamic and aeroelastic character of a flexible high speed civil transport wing. Data was acquired for the purpose of code validation and trend evaluation for this type of wing. The report describes a number of activities in preparing for and conducting the wind-tunnel test. These included coordination of the design and fabrication, development of analytical models, analysis/hardware correlation, performance of laboratory tests, monitoring of model safety issues, and wind-tunnel data acquisition and reduction. Descriptions and relevant evaluations associated with the pretest data are given in sections 1 through 6, followed by pre- and post-test flutter analysis in section 7, and the results of the aerodynamics/loads test in section 8. Finally, section 9 provides some recommendations based on lessons learned throughout the FSM program. |
| NASA分類 | Aerodynamics |
| レポートNO | NASA/CR-1999-209556
NAS 1.26:209556 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/227732 |
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