机译:垂直起降飞机降落的喷气夹带理论
Lockheed Martin Aeronautics Company, Palmdale, California 93599 Advanced Development Programs, 1011 Lockheed Way MS 1122;
Lockheed Martin Aeronautics Company, Palmdale, California 93599 1011 Lockheed Way;
Lockheed Martin Aeronautics Company, Palmdale, California 93599 Propulsion Airfrarae Integration, 1011 Lockheed Way;
A_j: jet exit area, ft~2; C: doublet strength, ft~2/s; C_p: pressure coefficient, (p-p_(ref))/q; D: plate diameter, ft; d: jet diameter, ft;
机译:垂直起降飞机降落的喷气夹带理论
机译:电动垂直起飞和着陆飞机电池的挑战和关键要求
机译:飞机垂直起降
机译:垂直起降飞机降落的喷气夹带理论
机译:垂直起降飞机的混合电动分布式推进器
机译:GNSS / INS和光学传感器在草地上确定飞机起飞和着陆性能的应用
机译:喷气襟翼作为垂直起降飞机升力发生器的可行性