Wide-range single engine operated from subsonic to hypersonic conditions: Designed by computational fluid dynamics

Ken Naitoh*, Kazushi Nakamura, Takehiro Emoto, Takafumi Shimada

*この研究の対応する著者

研究成果: Conference contribution

5 被引用数 (Scopus)

抄録

A new type of single engine capable of operating over a wide range of Mach numbers from subsonic to hypersonic regimes is proposed for airplanes. Traditional piston engines, turbojet engines, and scram engines work only under a narrower range of operating conditions. The new engine has no compressors or turbines such as those used in conventional turbojet engines. A notable feature is its system of super multijets that collide to compress gas for the transonic regime. A numerical model simulating compressible turbulence with chemical reactions based on the CIP and BI-SCALES methods is employed to design the engine. The maximum power of this engine will be sufficient for actual use. For the higher Mach numbers in supersonic and hypersonic conditions, this engine can take the mode of a ram or scramjet engine.

本文言語English
ホスト出版物のタイトルComputational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010
出版社Kluwer Academic Publishers
ページ763-768
ページ数6
ISBN(印刷版)9783642178832
DOI
出版ステータスPublished - 2011
イベント6th International Conference on Computational Fluid Dynamics, ICCFD 2010 - St. Petersburg, Russian Federation
継続期間: 2010 7月 122010 7月 16

出版物シリーズ

名前Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010

Conference

Conference6th International Conference on Computational Fluid Dynamics, ICCFD 2010
国/地域Russian Federation
CitySt. Petersburg
Period10/7/1210/7/16

ASJC Scopus subject areas

  • 流体および伝熱

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