Numerical study on the trajectory of a long-range flexible rocket with large slenderness ratio
Y Wang, M Xu, X An, Z Xu, W Xu, E Quan - Aerospace Science and …, 2021 - Elsevier
With the requirements of the speed, maneuverability and agility, the structure with large
slenderness ratio is widely employed in the design of the modern rocket. The interaction …
slenderness ratio is widely employed in the design of the modern rocket. The interaction …
[引用][C] Transient Aerodynamic Heating Effects on Aeroelastic Dynamic Response of Curved Fiber-Reinforced Composite Panel in Supersonic Airflow
Y Liu, J Duan, B Xu, J Wu - International Journal of Structural …, 2024 - World Scientific
The nonlinear aero-thermo-elastic behaviors of the curved-fiber composite panel are studied
accounting for transient aerodynamic heating effects with two-way coupling method. The …
accounting for transient aerodynamic heating effects with two-way coupling method. The …