| タイトル | Analytical procedures for flutter model development and checkout in preparation for wind tunnel testing of the DAST ARW-1 wing |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830007046 |
| 著者（英） | Pines, S. |
| 著者所属（英） | Analytical Mechanics Associates, Inc. |
| 発行日 | 1982-12-01 |
| 言語 | eng |
| 内容記述 | A study to develop analytical procedures to be used in the checkout and calibration of a flutter wind tunnel model of the DAST ARW-1 wing equipped with a flutter suppression device is reported. The methods used to obtain a realistic simulation of the structural inertial and aerodynamic properties of the wing, the hydro-electro-servo actuator used for flutter suppression, a prediction of the open loop flutter speed at a fixed Mach number (.897), a procedure for checkout and calibration using the method frequency response of a wing mounted accelerometer, and an analytical representation of a reduced state approximation of the overall system are described. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 83N15317
NAS 1.26:166023
NASA-CR-166023
AMA-82-35 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/163904 |
