Numerical investigation of dynamic stall suppression of rotor airfoil via improved co-flow jet-Reference-Cited by-同舟云学术

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Numerical investigation of dynamic stall suppression of rotor airfoil via improved co-flow jet

Published:2022-03 Issue:3 Volume:35 Page:169-184
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Liu Jiaqi,Chen Rongqian,You Yancheng,Shi Zheyu

Funder

National Natural Science Foundation of China

China Aerodynamics Research and Development Center

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference40 articles.

1. Principles of helicopter aerodynamics with CD extra;Leishman,2006761

2. Modern helicopter rotor aerodynamics;Conlisk;Prog Aerosp Sci,2001

3. Numerical investigation of compressibility effect on dynamic stall;Kim;Aerosp Sci Technol,2020

4. A review of helicopter rotor blade tip shapes;Brocklehurst;Prog Aerosp Sci,2013

5. A study on aerodynamic and acoustic characteristics of advanced tip-shape rotors;Zhao;J Am Helicopter Soc,2007

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