Author:
MA Li,ZHAO Qijun,ZHANG Kai,ZHANG Xiayang,ZHAO Mengmeng
Subject
Mechanical Engineering,Aerospace Engineering
Reference26 articles.
1. Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance;Zhao;Chin J Aeronaut,2020
2. Aeroelastic stability analysis of a composite rotor blade;Hong;J Am Helicopter Soc,1985
3. Smith EC, Chopra I. Aeromechanical stability of helicopters with composite rotor blades in forward flight. Procedings of the 48th American Helicopter Society Annual Forum; 1992 June 3-5; Arizona,America. Phenix VFS society; p. 57–73.
4. An aeroelastic model for composite rotor blades with straight and swept tips;Friedmann;Int J Non Linear Mech,2002
5. A moderate deflection composite helicopter rotor blade model with an improved cross-sectional analysis;Friedmann;Int J Solids Struct,2009
Cited by
12 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献