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An preliminary overview analysis on the internal waverider inlets for ramjet

  • Nanjing University of Aeronautics and Astronautics

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

11 引用 (Scopus)

摘要

Challenges and advantages of inward turning inlets for ramjet is investigated in this paper. Based on the qualitative and quantitative analysis, the inward turning inlets in ramjet field have following substantial advantages. 1) higher mass airflow capture, 2) shorter compressive length, 3) lower wetted area, 4) lower pressure drag, 5) lower skin friction drag. In detail, comparing to two-dimensional classical compression in ramjet, the total pressure recovery of ICFC inward-turning compression increases 28.0%; the compressive length decreases 5%; the wetted area decreases 15.7% and the pressure drag decreases 12.1%. In addition, the different throat Mach number between ramjet and scramjet of inward turning inlet makes the self-starting ability for ramjet facing more difficulty challenge. Furthermore, the inward turning inlets face more difficulty challenge than traditional inlets in ramjet field.

源语言英语
主期刊名21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624104633
出版状态已出版 - 2017
已对外发布是
活动21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 - Xiamen, 中国
期限: 6 3月 2017 → 9 3月 2017

丛书

姓名21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017

会议

会议21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
国家/地区中国
市Xiamen
时期6/03/17 → 9/03/17

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