| タイトル | UH-60 Airloads Program Tutorial |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090036797 |
| 著者（英） | Bousman, William G. |
| 著者所属（英） | Monterey Technologies, Inc. |
| 発行日 | 2009-05-27 |
| 言語 | eng |
| 内容記述 | From the fall of 1993 to late winter of 1994, NASA Ames and the U.S. Army flew a flight test program using a UH-60A helicopter with extensive instrumentation on the rotor and blades, including 242 pressure transducers. Over this period, approximately 30 flights were made, and data were obtained in level flight, maneuver, ascents, and descents. Coordinated acoustic measurements were obtained with a ground-acoustic array in cooperation with NASA Langley, and in-flight acoustic measurements with a YO-3A aircraft. NASA has sponsored the creation of a "tutorial' which covers the depth and breadth of the flight test program with a mixture of text and graphics. The primary purpose of this tutorial is to introduce the student to what is known about rotor aerodynamics based on the UH-60A measurements. The tutorial will also be useful to anyone interested in helicopters who would like to have more detailed knowledge about helicopter aerodynamics. |
| NASA分類 | Aerodynamics |
| レポートNO | ARC-E-DAA-TN517 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/252710 |
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