Tail Shells Supersonic Aerodynamic Characteristics Calculation And Analysis

This paper is to find a general way to quickly and relative precisely get the aerodynamic characteristics of a wing-body-tail combination at supersonic speeds.The theories and calculating process based on parts combination empirical methods were elaborately discussed,which were used to calculate the aerodynamic characteristics of projectiles,wings and wing-body-tail combinations.The program was made and the flow chart was drawn.In addition,the program was used to discuss and validate some aerodynamic phenomena,and was used to calculate several models.In the end,the results was analyzed and compared with experimental results to evaluate the program's application value and limitation.