Unsteady analysis of hot streak migration in a turbine stage
Author:
Affiliation:
1. United Technologies Research Center, East Hartford, Connecticut 06108
2. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23507
Reference15 articles.
1. Redistribution of an inlet temperature distortion in an axial flow turbine stage
2. Navier-Stokes analyses of the redistribution of inlet temperature distortions in a turbine
3. Numerical investigation of hot streaks in turbines
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