Numerical Investigation of the Effect of the Cavity on Flow Control of Continuous Pulses Opposing Plasma Synthetic Jets in Hypersonic Flow-Reference-Cited by-同舟云学术

Numerical Investigation of the Effect of the Cavity on Flow Control of Continuous Pulses Opposing Plasma Synthetic Jets in Hypersonic Flow

Published:2024-09 Issue:5 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Li Jiawei¹^ORCID,Chi Shaoqing²,Sun Zhikun³^ORCID

Affiliation:

1. Director, Yangzhou Collaborative Innovation Research Institute Co., Ltd., Building B, Building 28, Jiangsu Information Service Industry Base, Guangling New Town, Yangzhou City, Jiangsu Province 225000, China. ORCID: .

2. Lecturer, Dept. of Aeronautics and Astronautics, Shenyang Aerospace Univ., Shenyang 110136, China (corresponding author).

3. Lecturer, Dept. of Mechanical and Electrical Engineering, Suqian Univ., Suqian 223800, China. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5312

Reference25 articles.

1. Plasma Jet for Flight Control

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3. Cybyk B. K. Grossman and D. Van Wie. 2003. “Computational assessment of the SparkJet flow control actuator.” In Proc. 33rd AIAA Fluid Dynamics Conf. and Exhibit. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3711.

4. Cybyk B. K. Grossman and J. Wilkerson. 2004. “Performance characteristics of the SparkJet flow control actuator.” In Proc. 2nd AIAA Flow Control Conf. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2131.

5. Cybyk B. K. Grossman J. Wilkerson J. Chen and J. Katz. 2005. “Single-pulse performance of the SparkJet flow control actuator.” In Proc. 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-401.