Abstract

Computations were performed to study the three‐dimensional flow and heat transfer in a U‐shaped duct of square cross section with inclined ribs on two opposite walls under rotating and non‐rotating conditions. Two extreme limits in the Reynolds number (25,000 and 350,000) were investigated. The rotation numbers investigated are 0, 0.24, and 0.039. Results show rotation and the bend to reinforce secondary flows that align with it and to retard those that do not. Rotation was found to affect significantly the flow and heat transfer in the bend even at a very high Reynolds number of 350,000 and a very low Rotation number of 0:039. When there is no rotation, the flow and heat transfer in the bend were dominated by rib‐induced secondary flows at the high Reynolds number limit and by bend‐induced pressure‐gradients at the low Reynolds number limit. Long streaks of reduced surface heat transfer occur in the bend at locations where streamlines from two contiguous secondary flows merge and then flow away from the surface. The location and size of these streaks varied markedly with Reynolds and rotation numbers.This computational study is based on the ensemble‐averaged conservation equations of mass, momentum (compressible Navier‐Stokes), and energy. Turbulence is modelled by the low‐Reynolds shear‐stress transport (SST) model of Menter. Solutions were generated by using a cell‐centered, finite‐volume method, that is based on second‐order accurate flux‐difference splitting and a diagonalized alternating‐direction implicit scheme with local time‐stepping and V‐cycle multigrid.

Highlights

  • To increase thermal efficiency and specific thrust, advanced gas turbine stages are being designed to operate at gas temperatures that exceed acceptable material temperatures

  • Results show in detail the evolution of the secondary flows induced by inclined ribs

  • The cooler the fluid is near the surface

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Summary

Introduction

To increase thermal efficiency and specific thrust, advanced gas turbine stages are being designed to operate at gas temperatures that exceed acceptable material temperatures. Even with the development of thermal-barrier coatings, cooling is needed for all surfaces that come in contact with the hot gases, especially in the first stage. SHIH et al. One effective and widely used method of cooling is internal cooling. Lowertemperature air is extracted from the compressor and circulated through passages embedded inside components such as blades and vanes. Efficiency considerations demand effective cooling with minimal cooling air. This need for efficiency has led numerous investigators to study fluid flow and heat transfer processes inside internal coolant passages and to develop and evaluate design concepts that enhance heat transfer with minimal drag

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