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| 非均匀流等压比变后掠角高超侧 压 式 进 气 道 研 究 | |
| 摘 要： | |
INVESTIGATION OFSIDEWALL COMPRESSION INLET WITH CONSTANT PRESSURE RATION AND CURVED LEADING EDGE UNDERNONUNIFORM SUPERSONIC FLOW |
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| Fig.. INVESTIGATION OFSIDEWALL COMPRESSION INLET WITH CONSTANT PRESSURE RATION AND CURVED LEADING EDGE UNDERNONUNIFORM SUPERSONIC FLOW[J]. Journal of Propulsion Technology, 1999, 20: 1max-p21min | |
| Authors: | Fig. |
| Abstract: | |
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