Passive Control of Steady Condensation Shock Wave

查看全文 作　　者：[1]ShigeruMatsuo;[2]ShenYu;等

机构地区：[1]DepartmentofMechanicalEngineering,SagaUniversity,1,Honjo-machi,Saga-shi,Saga,840-8502,Japan;[2]InstituteofEngineeringThermophysics,ChineseAcademyofSciences,P.O.Box2706,Beijing100080,China

出　　处：《Journal of Thermal Science》索引2000年第9卷第4期,共6页

摘　　要：When condensation occurs in supersonic flow fields, the flow is affected by the latent heat released, and if the heat released exceeds a certain quantity, a condensation shock wave will occur There are many papers for the passive control of shock-boundary layer interaction using the porous wall with a plenum underneath on the application of the technique to transonic airfoil flows. In the present study, this passive technique is applied to the control of a steady condensation shock wave generated in a supersonic nozzle. In order to clarify the effect of the passive shockboundary layer control on condensation shock, Navier-Stokes equations were solved numerically using a 3rd-order MUSCL type TVD finite-difference scheme with a second-order fractional-step for time integration. As a result, the simulated flow fields were compared with experimental data in good agreement and the aspect of the flow field has been clarified. 关键词：喷嘴稳定冷凝冲击波控制

相关文献

参考文献（2）
引证文献（1）
耦合文献（6）

参考文献(2)

引证文献(1)

耦合文献(6)

互联网出版许可证新出网证(渝)字10号全国400电话 - 免长途话费

Passive Control of Steady Condensation Shock Wave

参考文献(2)

引证文献(1)

耦合文献(6)

用户提示