By using the method of aircraft and turbofan engine integrated analysis, a model of maneuverable missile and turbofan engine integrated optimum design was developed and the computational examples and the analysis were presented.
英
美
- 摘要利用飛機/渦扇發(fā)動(dòng)機一體化設計的思路，建立了飛航導彈/渦扇發(fā)動(dòng)機一體化設計的優(yōu)化設計模型并給出了算例和分析。
