Heat Transfer and Temperature Analysis of an Aeroengine Strut Under Icing Conditions-Reference-Cited by-同舟云学术

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Heat Transfer and Temperature Analysis of an Aeroengine Strut Under Icing Conditions

Published:2015-01 Issue:1 Volume:52 Page:216-225
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Dong W.¹,Zhu J.¹,Zhou Zhixiang²,Chi X.³

Affiliation:

1. School of Mechanical Engineering, Shanghai Jiaotong University, 200240 Shanghai, People’s Republic of China

2. AVIC Aviation Powerplant Research Institute, 412002 Zhuzhou, People’s Republic of China

3. School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana 47906

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032107

Reference29 articles.

1. Efficiency of a bleed air powered inlet icing protective system

2. AI-KhalilK. M.MillerD.WrightW. B. “Validation of NASA Thermal Ice Protection Computer Codes. III—The Validation of ANTICE,” AIAA Paper 1997-0051, 1997.

3. LEWICE 2.2 Capabilities and thermal validation

4. Verification and Validation of NASA LEWICE 2.2 Icing Software Code

5. Toward Real-Time Aero-Icing Simulation of Complete Aircraft via FENSAP-ICE

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