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Articles

Effect of the Combustor Wall on the Aerothermal Field of a Nozzle Guide Vane

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By Mälardalen, Ioanna Aslanidou, Budimir Rosic, Osney Thermofluids Laboratory
| Mechanical Engineering Magazine Verified
In gas turbines with can combustors, the trailing edge (TE) of the combustor transition duct wall is found upstream of every second vane. This paper presents an experimental and numerical investigation of the effect of the combustor wall TE on the aerothermal performance of the nozzle guide vane. In the measurements carried out in a high-speed experimental facility, the wake of this wall is shown to increase the aerodynamic loss of the vane.
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