To simulate the physical progress of the aircraft flying at six-degree-of-freedom in the wind tunnel and achieve the aerodynamics,kinematics and flight-control coupling characteristics of the aircraft,the low speed wind tunnel free-flight test technique for powered sub-scale aircraft is studied.Based on the similarity criterion,a test platform is established in a largescale low speed wind tunnel.A dynamic sub-scale model which is unstable in longitudinal static stability is augmented according to flight con...
【更新日期】
2017-11-10
【分类号】
V211.74
【正文快照】
2.中国空气动力研究与发展中心,绵阳621000网络出版地址:http://hkxb.buaa.edu.cn/CN/html/20171006.html引用格式:岑飞,聂博文,刘志涛,等.低速风洞带动力模型自由飞试验[J].航空学报,2017,38(10):121214.CEN F,NIE B W,LIU Z T,et al.Low speed wind tunnel free-flight test
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