A new model for simulating the effect of fuel injection oscillation in burner on the performanceand aerodynamic stability of the multi-stage axial compressor system with inlet steady pressure distortion is established.
英
美
- 建立了一種穩態(tài)壓力畸變進(jìn)氣條件下，多級軸流壓縮系統對燃燒室燃油瞬時(shí)脈沖的氣動(dòng)響應及氣動(dòng)穩定性分析的新方法；
