| 翻訳と辞書 |
| Miles M.11 Whitney Straight ： ウィキペディア英語版 |
Miles Whitney Straight
The Miles M.11 Whitney Straight was a 1930s British two-seat cabin monoplane with dual-controls.
==Design and development==
The M.11 Whitney Straight was designed by F.G. Miles of Philips and Powis as the result of collaboration with Whitney Straight, a Grand Prix motor racing driver, aviator and businessman. The aim was to provide comfortable accommodation for pilot, passenger and luggage in an enclosed 'side-by-side' cockpit. It was a low-wing monoplane, with fixed main undercarriage in aerodynamic fairings plus a fixed tailwheel. Construction was mainly of wood, with spruce frames and three-ply birch covering, and the wings had vacuum-operated split flaps. It was initially powered by a 130 hp (97 kW) de Havilland Gipsy Major I piston engine. The sole M.11B was powered by a 135 hp (101 kW) Amherst Villiers Maya I engine, adding 10 mph (16 km/h) to its maximum speed and 200 ft/min (60 m/min) to its rate of climb. A single M.11C was powered by a 145 hp (108 kW) de Havilland Gipsy Major II engine and variable-pitch propeller.〔Brown 1970, pp. 121-128〕〔Jackson 1988, pp. 62-65〕
thumb
thumb
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
■ウィキペディアで「Miles Whitney Straight」の詳細全文を読む
スポンサード リンク
| 翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|
.jpg){kind=link}
