2) turbofan jet
航空涡轮风扇发动机
3) fan-type aeroengine
扇形航空发动机
4) turbo shaft engine
航空涡轴发动机
1.
The traditional PID (Proportional-Integral-Differential) method, when used to control turbo shaft engine acceleration gives dynamic performance that is, in our opinion, not quite satisfactory.
研究了航空涡轴发动机加速过程的最优控制问题。
5) aviation turbojet engine
航空涡喷发动机
6) aero turbine engine
航空涡轮发动机
1.
The convergence problems of solving the nonlinear equations of aero turbine engines were study in detail,the common non-convergence cases were given and the mechanism was analyzed,based on Newton method,an advanced solutions for overcoming the common non-convergence problems was presented:variable step Newton method(VSN).
详细分析了航空涡轮发动机部件共同工作的非线性方程组的求解收敛性问题,并对计算中常见的迭代不收敛问题的机理进行了研究总结。
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条