Experimental Study on the Dynamic Characteristics and Surface Arc Plasma Control of Shock Train in the Supersonic Inlet-Reference-Cited by-同舟云学术

Experimental Study on the Dynamic Characteristics and Surface Arc Plasma Control of Shock Train in the Supersonic Inlet

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:

Kong Yakang¹,Li Jun²,Liang Hua²,Guo Shanguang³

Affiliation:

1. Master’s, Science and Technology on Plasma Dynamic Laboratory, Air Force Engineering Univ., No. 1 Baling Rd., Baqiao District, Xi’an 710038, China.

2. Professor, Science and Technology on Plasma Dynamic Laboratory, Air Force Engineering Univ., No. 1 Baling Rd., Baqiao District, Xi’an 710038, China.

3. Professor, Science and Technology on Plasma Dynamic Laboratory, Air Force Engineering Univ., No. 1 Baling Rd., Baqiao District, Xi’an 710038, China (corresponding author).

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.1943-5525.0001470

Reference47 articles.

1. Application of POD on time-resolved schlieren in supersonic multi-stream rectangular jets

2. Structure of self-excited oscillations in transonic diffuser flows

3. Navier-Stokes solutions for mixed compression axisymmetric inlet flow with terminal shock

4. Fluid Phenomena in Scramjet Combustion Systems

5. Unsteadiness characterization of shock wave/turbulent boundary layer interaction controlled by high-frequency arc plasma energy deposition

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