| 弹用涡喷发动机风车起动过程仿真及性能分析 |
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| 引用本文： | 杨欣毅,沈伟,刘海峰,董可海,王永华.弹用涡喷发动机风车起动过程仿真及性能分析[J].兵工学报,2011,32(1):37-44. |
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| 作者姓名： | 杨欣毅 沈伟 刘海峰 董可海 王永华 |
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| 作者单位： | （海军航空工程学院 飞行器工程系， 山东 烟台 264001） |
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| 摘 要： | 针对弹用涡喷发动机风车起动过程的特点,提出一种仿真求解机制:点火前的风车过程利用径向基函数神经网络(RBFN)方法建模仿真;点火后的加速过程则采用部件匹配法建立发动机动态模型仿真求解.动态模型的非线性方程组,利用粒子群优化算法(PSO)求解,解决了传统迭代解法受初值影响不易收敛的问题.计算结果与试验数据吻合较好,证明所...
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| 关 键 词： | 航空、航天推进系统 导弹推进 涡轮喷气发动机 风车 滑动最小二乘 粒子群算法 加速性能 |
Numerical Simulation and Performance Analysis on Start Process of Missile Turbojet Engine Windmill |
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| YANG Xin-yi,SHEN Wei,LIU Hai-feng,DONG Ke-hai,WANG Yong-hua.Numerical Simulation and Performance Analysis on Start Process of Missile Turbojet Engine Windmill[J].Acta Armamentarii,2011,32(1):37-44. |
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| Authors: | YANG Xin-yi SHEN Wei LIU Hai-feng DONG Ke-hai WANG Yong-hua |
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| Affiliation: | (Department of Aircraft Engineering， Naval Aeronautical and Astronautical University， Yantai 264001， Shandong， China) |
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| Abstract: | A new simulation strategy was proposed for the start process of missile turbojet engine windmill according to its characteristic.The simulation consists of two phases: the windmill process before ignition and the acceleration process after ignition.The former is simulated using radial basis function networks(RBFN),and the latter which model is a set of nonlinear equations is solved using particle swarm optimization(PSO) algorithm.The introduction of PSO helps to solve the divergence problem of nonlinear equ... |
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| Keywords: | propulsion system of aviation & aerospace missile propulsion turbojet engine windmill moving least square particle swarm optimization acceleration performance |
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