| タイトル | Pressure distribution data from tests of 2.29-meter (7.5-ft.) span EET high-lift research model in Langley 4- by 7-meter tunnel |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840020670 |
| 著者（英） | Morgan, H. L., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-06-01 |
| 言語 | eng |
| 内容記述 | A 2.29 m (7.5 ft.) span high-lift research model equipped with full-span leading-edge slat and part-span double-slotted trailing-edge flap was tested in the Langley 4- by 7-Meter Tunnel to determine the low speed performance characteristics of a representative high aspect ratio suprcritical wing. These tests were performed in support of the Energy Efficient Transport (EET) program which is one element of the Aircraft Energy Efficiency (ACEE) project. Static longitudinal forces and moments and chordwise pressure distributions at three spanwise stations were measured for cruise, climb, two take-off flap, and two landing flap wing configurations. The tabulated and plotted pressure distribution data is presented without analysis or discussion. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84N28739
NASA-TM-83111
NAS 1.15:83111 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/158979 |
