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kongqiliuliang
- 该程序计算航空发动机涡轮风扇的空气流量与风扇增压比的关系，各个符号参数均在程序中有说明-The program calculates the aero-engine turbo-fan air flow and fan pressure ratio relationship, each symbol parameters are described in the program
blade_strength_calculation
- 实现发动机涡轮叶片强度的简单计算，绘制相关曲线。(A simple calculation of engine turbine blade strength is realized, and the correlation curve is drawn.)
two
- 用于计算过航空涡轮喷气发动机热力学设计与计算(Thermodynamic Design and Computation for Calculating Aero Turbojet Engine)
engin homework
- 航空涡扇发动机设计点热力计算，适用于民用大涵道比燃气涡轮风扇发动机的热力计算。(Thermodynamic calculation of design point of aero-turbofan engine)