Heat-Transfer Coefficients of a Turbine Blade-Tip and Near-Tip Regions-Reference-Cited by-同舟云学术

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Heat-Transfer Coefficients of a Turbine Blade-Tip and Near-Tip Regions

Published:2003-07 Issue:3 Volume:17 Page:297-303
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Kwak Jae Su¹,Han Je-Chin¹

Affiliation:

1. Texas A&M University, College Station, Texas 77843-3123

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.6776

Reference21 articles.

1. The Influence of Turbine Clearance Gap Leakage on Passage Velocity and Heat Transfer Near Blade Tips: Part I—Sink Flow Effects on Blade Pressure Side

2. The Influence of Turbine Clearance Gap Leakage on Passage Velocity and Heat Transfer Near Blade Tips: Part II—Source Flow Effects on Blade Suction Sides

3. Cavity Heat Transfer on a Transverse Grooved Wall in a Narrow Flow Channel

4. Heat Transfer in the Tip Region of Grooved Turbine Blades

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