首页> 美国政府科技报告 >Inlet Spillage Drag Tests and Numerical Flow-Field Analysis at Subsonic and Transonic Speeds of a 1/8-Scale, Two-Dimensional, External-Compression, Variable-Geometry, Supersonic Inlet Configuration
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Inlet Spillage Drag Tests and Numerical Flow-Field Analysis at Subsonic and Transonic Speeds of a 1/8-Scale, Two-Dimensional, External-Compression, Variable-Geometry, Supersonic Inlet Configuration

机译:在1/8刻度,二维,外压缩,可变几何,超音速进气道配置的亚音速和跨音速速度下的进气泄漏阻力测试和数值流场分析

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摘要

Accurate spillage drag and pressure data are presented for a realistic supersonic inlet configuration. Results are compared with predictions from a finite-differencing, inviscid analysis computer procedure. The analytical technique shows good promise for the evaluation of inlet drag, but necessary refinements were identified. A detailed description of the analytical procedure is contained in the Appendix. (Author)

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