下颔式进气道实验研究
Experimental Investigation of Chin Inlet
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摘要: 为了验证下颔式进气道 /前机身一体化设计方案的合理性及其进气道性能, 对下颔式进气道 /前机身一体化设计方案进行了实验研究。测出了进气道总压恢复系数、畸变指数随流量系数、攻角、侧滑角的变化规律。结果表明, 进气道性能较好, 进气道 /发动机匹配良好。Abstract: In order to prove the reason of chin inlet/forebody integrated design and the performance of the inlet,the experimental investigation of the chin inlet configuration of a new design was done.In this experiment,Total pressure recovery (inlet efficiency) and pressure distortions at inlet varied with mass flow coefficient were measured.The experimental results show that this new design configuration is reasonable.Total pressure recovery and pressure distortions at the chin inlet are improved.Inlet/Forebody integration design is advantageous for aircraft.In the end,further improvement of the inlet is presented.
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Key words:
- inlet /
- integrated design /
- inlet/forebody matching /
- experimental investigation
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