Analysis of swirling flow effects on the characteristics of unsteady hot-streak migration

Author:

Wang Jingyu,Ge Ning,Sheng Chunhua

Funder

AECC Shenyang Engine Research Institute of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference20 articles.

1. Barringer MD, Thole KA, Polanka MD. Developing a combustor simulator for investigating high pressure turbine aerodynamics and heat transfer. In: ASME turbo expo 2004: power for land, sea, and air. Vienna: American Society of Mechanical Engineers; 2004. p. 565–75.

2. Effect of hot streak migration on unsteady blade row interaction in an axial turbine;Jenny;J Turbomach,2012

3. CFD investigation of the performance of a military HP axial turbine subjected to inlet temperature distortion;Zilli,2005

4. Analysis on the effect of a nonuniform inlet profile on heat transfer and fluid flow in turbine stages;Simone;J Turbomach,2012

5. Hot streak migration in a turbine stage: integrated design to improve aerothermal performance;Basol;J Eng Gas Turbines Power,2010

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