By CRC Press
Development at the good fortune of a longtime sequence of profitable meetings held each 4 years given that 1978, this booklet comprises the complaints of the eighth foreign convention on Turbochargers and Turbocharging. It offers the most recent applied sciences in relation to engine strain charging platforms from foreign and educational specialists within the box, protecting new advancements in compressors and novel consumption structures; more advantageous types for cycle simulation; electro strengthen platforms; tendencies and requisites; generators; and mechanical points reminiscent of thermomechanical research, dynamics, and axial load means.
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Additional info for 8th International conference on turbochargers and turbocharging
It has been demonstrated that the CFD process is a valid method of optimising inlet duct design. The flow conditioning devices, such as grillage, have shown to give improved compressor performance when tested on the engine, thus further validating the analytical process. 53 ACKNOWLEDGEMENT The authors would like to express their gratitude to Ford Motor Company for supporting this study and giving permission to publish this article. REFERENCES: [I] Effect of Air Inlet System on Compressor Operation.
2. The turbocharger and turbocharger housing used for the study are standard GT-20 frame size production units supplied by Honeywell Engine Boosting System. Whilst it is recognised that the performance of the compressor can be significantly influenced by the ducting between the compressor outlet and engine inlet manifold, the current study focuses only upon the effect of the turbocharger compressor inlet duct. It is intended that the current work be extended to include one-dimensional and threedimensional flow analysis of the outlet ducting.
The flow to be simulated is assumed to be steady state, isothermal, compressible and turbulent. The effects of turbulence on the flow are represented through the turbulent viscosity. For this study, the turbulent viscosity is calculated by using the 'High Reynolds number k-£ model' with wall function for closure. The first-order Upwind Differencing (UD) scheme is used for the momentum, energy and turbulence equations. 001. 3 Computational grid The geometry of the clean side air duct used in this study is shown in Fig.