| タイトル | Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model |
| 著者（英） | Farmer, Moses G.; Bennett, Robert M.; Rivera, Jose A.; Eckstrom, Clinton V.; Dansberry, Bryan E.; Seidel, David A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | The Structural Dynamics Division at NASA Langley Research Center has started a wind tunnel activity referred to as the Benchmark Models Program. The primary objective of the program is to acquire test data that will be useful for developing and evaluating aeroelastic type CFD codes currently in use of under development. This paper describes the progress achieved in testing the first model in the Benchmark Models Program. Experimental flutter boundaries are presented for a rigid semispan model (NACA 0012 airfoil section) mounted on a flexible mount system. Also, steady and unsteady pressure measurements taken at the flutter condition are presented. The pressure data were acquired over the entire model chord located at the 60 percent span station. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 91A31900
AIAA PAPER 91-1010 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/349051 |
