By using the method of aircraft and turbofan engine integrated analysis, a model of maneuverable missile and turbofan engine integrated constrain analysis and mission analysis was developed and the computative examples and the analysis were given.
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)機一體化設計的約束分析和任務(wù)分析模型并給出了算例和分析。
