Effects of Radial Location on the Migration of Hot Streaks in a Turbine
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035-1000
2. Virginia Commonwealth University, Richmond, Virginia 23284-3105
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/10.2514/2.5589
Reference21 articles.
1. Redistribution of an inlet temperature distortion in an axial flow turbine stage
2. Numerical investigation of hot streaks in turbines
3. Navier-Stokes analyses of the redistribution of inlet temperature distortions in a turbine
4. Unsteady Euler analysis of the redistribution of an inlet temperature distortion in a turbine
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1. Numerical Study of the Axial Gap and Hot Streak Effects on Thermal and Flow Characteristics in Two-Stage High Pressure Gas Turbine;Energies;2018-10-04
2. Influence of Mainstream Turbulence Intensity on Heat Transfer Characteristics of a High Pressure Turbine Stage With Inlet Hot Streak;Journal of Turbomachinery;2015-12-29
3. Effects of Hot Streak and Airfoil Clocking on Heat Transfer and Aerodynamic Characteristics in Gas Turbine;Journal of Turbomachinery;2015-11-03
4. Unsteady Analysis on the Effects of Tip Clearance Height on Hot Streak Migration Across Rotor Blade Tip Clearance;Journal of Engineering for Gas Turbines and Power;2014-02-28
5. Tip-Clearance Effects on Hot-Streak Migration in Low-Pressure Stage of Vaneless Counter-Rotating Turbine;Journal of Propulsion and Power;2009-07
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