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DELTOID MAIN WING AERODYNAMIC CONFIGURATIONS

机译:三角肌主翼气动配置

摘要

Deltoid Main Wing idea provides for several innovative aerodynamic configurations for large subsonic and supersonic civil and military aircraft including “T-tailed Deltoid Main Wing” configuration that allows for design of high-subsonic jumbo jet passenger aircraft with a capacity between 200 and 700 passengers whose outer dimensions fit within 80 m box on class VI airports while having more than twice lower fuel consumption per unit of payload when compared to the present classical-concept aircraft with the same passenger capacity, while further allowing for design of all-size and all-purpose, high-lift-capacity, and long-range unmanned aircraft.
机译:三角肌主翼构想为大型亚音速和超音速民用和军用飞机提供了几种创新的空气动力配置,其中包括“ T尾三角肌主翼”配置,可设计载有200至700名乘客的高亚音速超大型喷气客机外部尺寸适合于VI级机场的80 m盒子内,与具有相同载客量的现有经典概念飞机相比,每单位有效载荷的油耗降低两倍以上,同时还允许设计全尺寸和全尺寸飞机,用途,高升力和远程无人驾驶飞机。

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