analyzing existing engineering methods, we combine them in such a way to make computing aerodynamic characteristics possible for arbitrarily shaped body 驗證、分析了各種超音速、高超音速氣動力工程計算方法,將各種工程方法統一起來,用于求解任意外形的飛行器氣動力。
this paper mainly discusses the software's whole scheme design and the system realizing method, and how to pick up the shrapnel model's diagnostic parameters on the solidworks plane, and how to compute aerodynamic force and ballistic characteristic etc . the software package is produced with visual c + + 6.0 and c + + builder 5.0 本文主要論述了軟件的總體方案設計,系統實現方法,solidworks環境下榴彈實體模型的參數提取方法,氣動力計算、內外彈道仿真計算、威力計算、穩定性分析的模型建立與求解方法,運用visualc++6.0和c++builder5.0語言進行了軟件的具體設計。