Numerical investigation on the assistant restarting method of variable geometry for high Mach number inlet
| Autor: | Liu Yuan, Zhansen Qian, Lu Wang |
|---|---|
| Rok vydání: | 2018 |
| Předmět: |
Physics
Total internal reflection geography geography.geographical_feature_category Bubble Flow (psychology) Aerospace Engineering 02 engineering and technology Mechanics Physics::Classical Physics Critical value Inlet 01 natural sciences 010305 fluids & plasmas Physics::Fluid Dynamics symbols.namesake 020303 mechanical engineering & transports Amplitude 0203 mechanical engineering Mach number Drag 0103 physical sciences symbols |
| Zdroj: | Aerospace Science and Technology. 79:647-657 |
| ISSN: | 1270-9638 |
| DOI: | 10.1016/j.ast.2018.06.014 |
| Popis: | To compromise the compression efficiency and the starting properties, the inner contraction ratio (ICR) of a general high Mach number inlet is usually designed in the range of dual solution area. When going into an unstarted status, the high Mach inlet needs an assistant method to restart. This work explores a variable geometry method to restart the inlet. The rotating cowl is adopted to a typical Mach 4 cruising inlet, and the unsteady computation method with a dynamic Chimera grid technique is applied to simulate the rotating process of the inlet cowl. The change characteristics of the restarted performance at different rotating angle amplitude of the inlet cowl are investigated systematically. The numerical results reveal that the unstarted status of this typical inlet induced by the effect of high backpressure failed to restart if the inlet cowl rotating angle amplitude is under a small critical value, which is called lower critical angle. The inlet could restart if the cowl rotating angle amplitude is a little larger than the lower critical angle, and the flow may rapidly go to a steady condition after the inlet cowl returns to the design position. However, the performance of the restarted inlet is still worse than the design condition, because of the existence of an stable separation bubble on its shoulder, even if the inlet cowl stops rotating. The separation bubble becomes shrunk with an increasing the cowl rotating angle amplitude. When the inlet cowl rotating angle amplitude reaches a large critical value which is called upper critical angle, the separation bubble disappears, and all the separation is swallowed by the mean flow. Therefore the design performance of the inlet can be recovered, which means that the flow mass capture coefficient, total pressure recovery coefficient, drag and the outlet Mach number go back to the design level. It also shows that within the range of the lower and upper critical angles, the larger the rotating angle amplitude is, the more rapidly the separation bubble reaches stable state. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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