Lift Augmentation Potential of the Circulation Control Wing Driven by Sweeping Jets-Reference-Cited by-同舟云学术

Lift Augmentation Potential of the Circulation Control Wing Driven by Sweeping Jets

Published:2022-08 Issue:8 Volume:60 Page:4677-4698
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Li Ziyan^ORCID,Liu Yudan,Zhou Wenwu,Wang Shiqi¹,Wen Xin,Liu Yingzheng

Affiliation:

1. Aero-Engine Academy of China, 101304 Beijing, People’s Republic of China

Funder

Aeronautical Science Foundation of China

Science and Technology Commission of Shanghai Municipality

National Natural Science Foundation of China

Advanced Jet Propulsion Innovation Center

State Key Laboratory of Aerodynamics

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061456

Reference86 articles.

1. Applications of the Coanda Effect

2. Circulation control pneumatic aerodynamics: blown force and moment augmentation and modification - Past, present and future

3. An Active Flow Circulation Controlled Flap Concept for General Aviation Aircraft Applications

4. STOE Potential of the Circulation Control Wing for High-Performance Aircraft

5. SaeedB. “Exploring the Aerodynamic Characteristics of a Blown-Annular Wing for V/STOL Aircraft,” Ph.D. Thesis, Brunel Univ., Uxbridge, England, U.K. 2010, https://bura.brunel.ac.uk/handle/2438/5173.

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