Numerical Investigation on Flow Control of a Hypersonic Airfoil by Plasma Synthetic Jet-Reference-Cited by-同舟云学术

Numerical Investigation on Flow Control of a Hypersonic Airfoil by Plasma Synthetic Jet

Published:2022-09 Issue:5 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sun Zhikun¹^ORCID,Shi Zhiwei²^ORCID,Zhang Weilin³,Sun Qijie³,Sun Quanbing³,Li Zheng⁴

Affiliation:

1. Graduate Student, Dept. of Aeronautics and Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China. ORCID: .

2. Professor, Dept. of Aeronautics and Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China (corresponding author). ORCID: .

3. Graduate Student, Dept. of Aeronautics and Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

4. Researcher, Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, Beijing 100076, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001467

Reference36 articles.

1. Plasma Jet for Flight Control

2. Drag reduction of supersonic blunt bodies using opposing jet and nozzle geometric variations

3. Plasmas in high speed aerodynamics

4. Simulations of Nanosecond Pulsed Plasmas in Supersonic Flows for Combustion Applications

5. Chiatto M. and L. de Luca. 2017. “Numerical and experimental frequency response of plasma synthetic jet actuators.” In Proc. 55th AIAA Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1884.

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