Research on Propeller Icing Characteristics-Reference-Cited by-同舟云学术

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Research on Propeller Icing Characteristics

Published:2023-11-10 Issue: Volume:50 Page:1-6
ISSN:
Container-title:2023 17th Symposium on Piezoelectricity, Acoustic Waves, and Device Applications (SPAWDA)
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Author:

Li Bing¹,He Miao²,Lin Chen³,Zhou Zhihong³,Xiong Huajie³,Wu Zhulong³

Affiliation:

1. AVIC Huiyang Aviation Propeller Co., Ltd.,Baoding,China,071051

2. Military Representative Office in Baoding,Beijing Bureau of the Air Force Equipment Department,Baoding,China,071000

3. Sichuan University,Department of Mechanics & Engineering,Chengdu,Sichuan,P.R. China,610065

Funder

National Natural Science Foundation of China

National Science and Technology Major Project

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10412238/10412239/10412297.pdf?arnumber=10412297

Reference11 articles.

1. Numerical Study on the Influence of Three- Dimensional Ice Accretion on the Aerodynamic Characteristics of Propellers;Li;Machinery Manufacturing and Automation,2021

2. Research on Similarity Criteria for Propeller Icing Experiments. In;Yi

3. Numerical and Experimental Investigation of Ice Accretion on Rotorcraft Engine Air Intake

4. Computational simulation of ice accretion and shedding trajectory of a rotorcraft in forward flight with strong rotor wakes

5. Deicing of helicopter blades using piezoelectric actuators

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