| タイトル | Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930084843 |
| 著者（英） | Emery, James C; Erwin, John R; Herrig, L Joseph |
| 著者所属（英） | National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
| 発行日 | 1957-02-01 |
| 言語 | eng |
| 内容記述 | A two-dimensional low-speed porous-wall cascade tunnel investigation has been conducted to establish the performance of the NACA 65-series compressor blade sections over the useful range of inlet angle, solidity, and section camber. Design points for optimum high-speed operation are presented. The loading limitation is determined for some conditions. Trends of section operating range with increasing section camber are determined for the four inlet angles tested. |
| レポートNO | 93R14133
NACA-TN-3916 |
| 権利 | No Copyright |
