| タイトル | Small transport aircraft technology propeller study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830020907 |
| 著者（英） | Rohrbach, C.; Black, B. M.; Magliozzi, B. |
| 著者所属（英） | Hamilton Standard |
| 発行日 | 1983-04-11 |
| 言語 | eng |
| 内容記述 | A study to define potential benefits of advanced technology propeller for 1985-1990 STAT commuter airplanes was completed. Two baselines, a Convair, 30 passenger, 0.47 Mach number airplane and a Lockheed, 50 passenger, 0.70 Mach number airplane, were selected from NASA-Ames sponsored airframe contracts. Parametric performance, noise level, weight and cost trends for propellers with varying number of blades, activity factor, camber and diameter incorporating blade sweep, tip proplets, advanced composite materials, advanced airfoils, advanced prevision synchrophasing and counter-rotation are presented. The resulting DOC, fuel burned, empty weight and acquisition cost benefits are presented for resizings of the two baseline airplanes. Six-bladed propeller having advanced composite blades, advanced airfoils, tip proplets and advanced prevision synchrophasers provided the maximum DOC improvements for both airplanes. DOC and fuel burned were reduced by 8.3% and 17.0% respectively for the Convair airplane and by 24.9% and 41.2% respectively for the Lockheed airplane. The larger reductions arose from a baseline definition with very heavy fuselage acoustic treatment. An alternate baseline, with a cabin noise 13dB in excess of the objective, was also studied. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 83N29178
NASA-CR-168045
HSER-8826
NAS 1.26:168045 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/162143 |
|
