... 多孔型纵槽表面 fluted surface with thin porous coatings 气动力优化设计 aerodynamic optimization design 汉字合并 chinese characters amalgamating ...
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以展弦比为8.6的机翼加装帆片为例,进行了气动力计算并作了帆片优化设计。
The aerodynamic computation and the design of optimized wing sails for aircraft with rectangular wing whose aspect ratio equals 8. 6 were completed.
为了优化无人驾驶航空飞行器在整个飞行过程中的空气动力特性而使机身、推进系统和升力控制面一体化的设计技术。
Design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces to optimize aerodynamic performance throughout the flight regime of an unmanned air vehicle.
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