Presents the use of the similar transform and potential theory for calculation of the bypass flow factor and pressure gradient and the analysis of the influence of bypass flow factor and pressure gradient on heat tran...Presents the use of the similar transform and potential theory for calculation of the bypass flow factor and pressure gradient and the analysis of the influence of bypass flow factor and pressure gradient on heat transfer is analyzed, and the distribution of nose cone ablation obtained by combining the controlling equations of boundary layer, the compatible relation of interface and the heat conduction of interior.展开更多
Presents the general physical mathematical model established for ablation of carbon carbon composite, a double moving boundary method used to determine the surface temperature, ablation rate and thickness of thermal p...Presents the general physical mathematical model established for ablation of carbon carbon composite, a double moving boundary method used to determine the surface temperature, ablation rate and thickness of thermal protection material and real time simulation of ablation at stagnation point of some missile between 65～20km during reentry.展开更多
文摘Presents the use of the similar transform and potential theory for calculation of the bypass flow factor and pressure gradient and the analysis of the influence of bypass flow factor and pressure gradient on heat transfer is analyzed, and the distribution of nose cone ablation obtained by combining the controlling equations of boundary layer, the compatible relation of interface and the heat conduction of interior.
文摘Presents the general physical mathematical model established for ablation of carbon carbon composite, a double moving boundary method used to determine the surface temperature, ablation rate and thickness of thermal protection material and real time simulation of ablation at stagnation point of some missile between 65～20km during reentry.
