Parametric effects in a scramjet engine on the interaction between the air stream and the injection
作者： W Huang , L Ma , M Pourkashanian , D B Ingham , S-B Luo
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摘要: The mixing of fuel and air in supersonic flow plays a significant role the enhancement performance scramjet engines. In this article, two-dimensional coupled implicit Reynolds-averaged Navier–Stokes equations standard k–e turbulent model are introduced to investigate interaction between helium stream injected into typical engine. A range different angles (30–150°) both incoming injection under various pressure conditions (0.62–1.86 MPa) have been investigated assess their impact on mixing. It is shown among cases studied for injections that an angle 90° produces highest efficiency. with variable angle, then situation 30° can achieve higher efficiency than other angles. addition, injection, mix better.
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sci-hub.se 参考文章(19)
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