عنوان مقاله :
شبيه سازي عددي خنك كاري لايه اي سه بعدي آشفته غير قابل تراكم با استفاده از رهيافت هاي RANS و LES
عنوان به زبان ديگر :
Three-dimensional Turbulent Incompressible Film Cooling Simulation,Using LES and RANS Approaches
پديد آورندگان :
طيبي رهني ، محمد نويسنده Taeibi-Rahni, mohammad
اطلاعات موجودي :
فصلنامه سال 1384 شماره 3
كليدواژه :
شبيه سازي گردابه هاي بزرگ , مهندسي , پره هاي توربين هاي گاز , LES , Film Cooling , Turbulence modeling , Large eddy simulation , Finite volume method , خنك كازي لايه اي , Gas Turbine Blades , مدل سازي آشفتگي , RANS
چكيده لاتين :
Film cooling has many applications such as in the gas turbine blade cooling, where inhales are introduced in the blades from which the cooling fluid are injected to the main stream covers the blade surface. In this research, turbulent three-dimensional film cooling over a flat plate is numericallying investigated. Reynolds-averaged Navier-Stokes approach is applied for the simulations, using the standard k - e and shear stress transport models. Also, the simulations are performed using large eddy simulation approach with the Smagorinsky subgrid scale model. The finite volume method and the SIMPLE algorithm are applied in both simulations and the spatial and temporal terms are discretized using the power-law and the Crank-Nicolson schemes, respectively. At 90° injection angle, the results are compared with previous experimental and numerical results showing close agreements. Optimum values of velocity ratio and injection angle are obtained using the film cooling effectiveness Parameta.
عنوان نشريه :
مكانيك هوافضا
عنوان نشريه :
مكانيك هوافضا
اطلاعات موجودي :
فصلنامه با شماره پیاپی 3 سال 1384
كلمات كليدي :
#تست#آزمون###امتحان