Experimental Study on Icing and Anti-Icing Characteristics of Engine Inlet Guide Vanes
Author:
Affiliation:
1. School of Mechanical Engineering, Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China
2. AVIC Aviation Power Plant Research Institute, 412002 Zhuzhou, People’s Republic of China
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/10.2514/1.B35679
Reference41 articles.
1. Aircraft engine anti-icing test and evaluation technology
2. Efficiency of a bleed air powered inlet icing protective system
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4. Further Refinement of the LEWICE SLD Model
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