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- The pressure field measurement results on the wing surface of airplane model by luminescence pressure sensor (LPS) technique and classic tap technique in high speed wind tunnel are presented. 介绍了国内首次在高速风洞中使用荧光压力传感器(LPS)技术对飞机模型机翼表面压力场测量的初步结果。
- Preliminary research on super-high angle of attack test techniques in a high speed wind tunnel 高速风洞超大迎角试验技术初步研究
- Computational investigation of longitudinal support interferences in high speed wind tunnel 高速风洞支架干扰数值修正研究
- Simulated test technique for engine air intake and exhaust in high speed wind tunnel 高速风洞发动机进排气动力模拟试验技术
- Investigation of high speed wind tunnel test technology for aerodynamics compensation airspeed heads 气动补偿空速管高速风洞试验技术研究
- Experimental investigation on aircraft component and external-stores force-measurement in high speed wind tunnel 高速风洞飞机部件和外挂物同时测力试验研究
- Investigation on dynamic force tests for the stabilizing parachute of the ejection seat in high speed wind tunnel 弹射座椅稳定伞高速风洞动态测力试验研究
- A new control system of CTS device and its application in 1.2m high speed wind tunnel 2m高速风洞CTS装置新控制系统及其应用研究
- Balance development of XX torpedo using the rocket-boosting in the separation test of the torpedo and the rocket in high speed wind tunnel XX型火箭助飞鱼雷雷箭分离高速风洞试验测力天平研制
- Pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel 在高速风洞中使用荧光压力传感器技术对飞机模型压力场的实验研究
- high speed wind tunnel 高速风洞
- This paper describes the progr ess obtained on the half model testing technique research in high speed adaptive wall wind tunnel in Northwestern Polytechnical University (NPU). 为了克服自适应壁风洞在模型支撑方面的困难和加大试验模型，提高试验雷诺数，西北工业大学在高速二元柔壁自适应壁风洞中开展了半模型试验技术的研究。
- CORRELATION STUDY ON FORCE TEST DATA FOR AIRCRAFT AT HIGH ANGLES OF ATTACK IN 1.2m AND 0.6m HIGH SPEED WIND TUNNELS 2m和0.;6m高速风洞飞机大攻角测力试验数据相关性研究
- Detailed flow field measurements were conducted in a low speed wind tunnel for both original and modified LGV's which are used in turbofan engines. 采用实验方法对某型弹用涡扇发动机涡轮低压导向器原型和改型进行了详细的低速风洞实验。
- Research is conducted on the energy loss of flow around a cascade of guide vanes in a low speed wind tunnel numerically and experimentally. 低速回流式风洞中拐角部位的流动损失占总损失的比重很大,该位置导流片绕流的流动状况对于流动损失有明显的影响。
- Finally, OL in the varied speed wind tunnel is also investigated.Results show that the actual opening process can be well simulated. 同时，变速风洞的伞衣载荷研究表明，变速风洞可较好地模拟实际开伞情况。
- Investigation of dynamic test technology for a model pitching oscillation with large amplitude in high speed wind tunnels 高速风洞大振幅俯仰动态试验技术研究
- This paper describes the investigation of boundary layer separation control for supercritical aerofoil using micro vortex generator in the low speed wind tunnel. 在低速风洞中研究了微型涡流发生器对超临界翼型边界层分离的控制。
- Force and PIV local flow measurements were conducted in a low speed wind tunnel to study the effectiveness of serrated Gurney flap at different deflections. 用低速风洞测力试验和襟翼处绕流的PIV测量试验研究锯齿形格尼襟翼在不同偏角下的增升效益.
- Wind tunnel experiments on aerodynamics of quasi high speed trains driven respectively by a diesel locomotive, Dongfeng 11, and by an electric locomotive, Shaoshan 8, are conducted. 介绍了以东风11型内燃机车牵引的准高速列车风洞模型试验，包括以韶山8型电力机车作牵引的对比试验。
