摘要: An axisymmetric air intake system for a jet aircraft engine comprising a fixed cowl extending outwardly from the face of the engine, a centerbody coaxially disposed within the cowl, and an actuator for axially displacing the cente... 展开
作者 | Sorensen, N. E. | ||
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原报告号 | 19770011210 | 总页数 | 9 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | ENGINE INLETS INTAKE SYSTEMS JET ENGINES ENGINE DESIGN |