Control of Stress in Aeroengine Turbine Disk Using Radially Rotating Heat Pipe-Reference-Cited by-同舟云学术

Control of Stress in Aeroengine Turbine Disk Using Radially Rotating Heat Pipe

Published:2014-07 Issue:3 Volume:28 Page:428-439
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Ding Shuiting¹,Luo Bin¹

Affiliation:

1. Beijing Key Laboratory on Safety of Integrated Aircraft and Propulsion Systems, National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Beihang University, 100191 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.T4235

Reference24 articles.

1. Development of Key Technologies for the Next Generation Gas Turbine

2. Failure analysis of turbine disc of an aero engine

3. Overview of FGM Research in Japan

4. Modeling and Analysis of Functionally Graded Materials and Structures

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