Effects of radial location on the migration of hot streaks in a 1-1/2 stage turbine
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
2. GMI Engineering and Management Inst., Flint, MI
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3578
Reference22 articles.
1. Redistribution of an inlet temperature distortion in an axial flow turbine stage
2. Hot Streaks and Phantom Cooling in a Turbine Rotor Passage: Part 1 — Separate Effects
3. Numerical investigation of hot streaks in turbines
4. Navier-Stokes analyses of the redistribution of inlet temperature distortions in a turbine
5. Navier-Stokes simulations of rotor/stator interaction using patched and overlaid grids
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. The influence of inlet swirl intensity and hot-streak on aerodynamics and thermal characteristics of a high pressure turbine vane;Chinese Journal of Aeronautics;2021-11
2. The Effects of High Mainstream Turbulence and Turbine Vane Film Cooling on the Dispersion of a Simulated Hot Streak;Journal of Turbomachinery;2004-01-01
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