TY - JOUR
T1 - 高超声速飞行器气动弹性的近期进展与发展展望
AU - Ye, Zhengyin
AU - Meng, Xianzong
AU - Liu, Cheng
AU - Ye, Liuqing
N1 - Publisher Copyright:
© 2018, The Editorial Board of Acta Aerodynamica Sinica. All right reserved.
PY - 2018/12/1
Y1 - 2018/12/1
N2 - The aeroelasticity (especially the aerothermoelasticity) of the high-speed aircraft is raising more and more attention in recent years. First of all, this paper summarizes the recent progress of the aeroelasticity problems according to different numerical methodologies. Then, based on the problems emerging in engineering practice, the thermal aeroelastic problems of high-speed vehicles are divided into issues related to thermal aeroelasticity of the aircraft and the thermal aeroelasticity of the inner runners, and their research status and future development are discussed. Particularly, the aerothermoelasticity problems related to the engine (including the panel flutter inside the ramjet engine and the aeroelasticity of the rocket engine nozzle) are investigated in detail and the significance of this issue in future work is pointed out.
AB - The aeroelasticity (especially the aerothermoelasticity) of the high-speed aircraft is raising more and more attention in recent years. First of all, this paper summarizes the recent progress of the aeroelasticity problems according to different numerical methodologies. Then, based on the problems emerging in engineering practice, the thermal aeroelastic problems of high-speed vehicles are divided into issues related to thermal aeroelasticity of the aircraft and the thermal aeroelasticity of the inner runners, and their research status and future development are discussed. Particularly, the aerothermoelasticity problems related to the engine (including the panel flutter inside the ramjet engine and the aeroelasticity of the rocket engine nozzle) are investigated in detail and the significance of this issue in future work is pointed out.
KW - Aerothermoelasticity
KW - Fluid-structure coupling
KW - Hypersonic speed vehicles
KW - Nozzles
KW - Scramjet
UR - http://www.scopus.com/inward/record.url?scp=85061248427&partnerID=8YFLogxK
U2 - 10.7638/kqdlxxb-2018.0060
DO - 10.7638/kqdlxxb-2018.0060
M3 - 文献综述
AN - SCOPUS:85061248427
SN - 0258-1825
VL - 36
SP - 984
EP - 994
JO - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
JF - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
IS - 6
ER -