| タイトル | Wind tunnel model and method |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740009842 |
| 著者（英） | Jackson, C. M., Jr.; Summerfield, D. G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1974-02-12 |
| 言語 | eng |
| 内容記述 | The design and development of a wind tunnel model equipped with pressure measuring devices are discussed. The pressure measuring orifices are integrally constructed in the wind tunnel model and do not contribute to distortions of the aerodynamic surface. The construction of a typical model is described and a drawing of the device is included. |
| NASA分類 | ELECTRONIC EQUIPMENT |
| レポートNO | 74N17955 |
| 権利 | No Copyright |
