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An preliminary overview analysis on the internal waverider inlets for ramjet

  • Nanjing University of Aeronautics and Astronautics

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

11 Scopus citations

Abstract

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.

Original languageEnglish
Title of host publication21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624104633
StatePublished - 2017
Externally publishedYes
Event21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 - Xiamen, China
Duration: 6 Mar 2017 → 9 Mar 2017

Publication series

Name21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017

Conference

Conference21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
Country/TerritoryChina
CityXiamen
Period6/03/17 → 9/03/17

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