Bi-global Linear Stability Analysis of Laminar Separation Bubble for Helicopter Blade Section Undergoing Dynamic Stall-Reference-Cited by-同舟云学术

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Bi-global Linear Stability Analysis of Laminar Separation Bubble for Helicopter Blade Section Undergoing Dynamic Stall

Published:2021-01-04 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2021 Forum
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Author:

Wen Guangwei¹,Gross Andreas¹

Affiliation:

1. New Mexico State University

Publisher

American Institute of Aeronautics and Astronautics

Reference51 articles.

1. Unsteady Airfoils

2. Numerical Investigation of Deep Dynamic Stall for a Helicopter Blade Section

3. Dynamic Stall Life Cycle on a Rotating Blade in Steady Forward Flight

4. Advance ratio effects on the flow structure and unsteadiness of the dynamic-stall vortex of a rotating blade in steady forward flight

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Laminar Separation Control for Eppler 387 Airfoil Based on Resolvent Analysis;AIAA Journal;2024-04

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