... and the single rotor system, and to comprehensively and specifically mention the method of generating the dynamic model. Next, based on the establishment of a dynamic model with and without SFD in the rotor system, the optimization design of the rotor system with SFD was carried out using a genetic algorithm...

... is proposed to optimize the honeycomb buffer of a legged-type lander. Optimization design variables are the dimension parameters of honeycomb and the objective functions are the evaluation parameters of the above two performance metrics. Design/methodology/approach A multi-body dynamic model of a lander...

...) was the first to use the adjoint method in fluid mechanics, and then Jameson (1988) applied adjoint method in the aeronautical field. Combining the continuous adjoint method with CFD technology, based on optimal control theory, Jameson developed what he calls optimal design method which is successfully...