| タイトル | Analysis of wake vortex flight test data behind a T-33 aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750015410 |
| 著者（英） | Jacobsen, R. A.; Kuhn, G. D. |
| 著者所属（英） | Nielsen Engineering and Research, Inc. |
| 発行日 | 1975-04-01 |
| 言語 | eng |
| 内容記述 | Measurements of the vortex system behind a T-33 aircraft were obtained by a Learjet equipped with a boom carrying a three-wire, hot-wire anemometry probe and other instrumentation. Analysis of the measurements using a computerized geometric method indicated the vortices had a core radius of approximately 0.11 meter with a maximum velocity of 25 meters per second. The hot-wire anemometer was found to be a practical and sensitive instrument for determining in-flight vortex velocities. No longitudinal instabilities, buoyant effects or vortex breakdowns were evident in the data which included vortex wake cross sections from 0.24 to 5.22 kilometers behind the T-33. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 75N23482
NASA-CR-137669
NEAR-TR-84 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/190097 |
