4   Artículos

 
en línea
Yu Tian, Luofeng Wang, Zhongliang Zhou and Renliang Chen    
In order to reveal the mechanism of Category II rotor-body-slung-load coupled oscillation (RBSLCO) with the frequency range of 2.5~8 Hz, a novel nonlinear rigid-elastic coupled model is presented for the helicopter and slung load system (HSLS) with expli... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ruhao Hua, Qi Chen, Zhao Wan and Hao Chen    
A body flap/RCS-integrated configuration is often used to achieve pitch trimming and controlled flight in near space for hypersonic vehicles. Under the high temperature and pressure load induced by the expansion wave at the nozzle exit, the body flap is ... ver más
Revista: Aerospace    Formato: Electrónico

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