Separated-Flow Control Simulation with a Periodic Excitation by SDBD Plasma Actuator at Re=O(205)-Reference-Cited by-同舟云学术

Separated-Flow Control Simulation with a Periodic Excitation by SDBD Plasma Actuator at Re=O(205)

Published:2020-11 Issue:6 Volume:33 Page:05020003
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Bernal-Orozco R. A.¹^ORCID,Arias-Montano Alfredo²,Huerta-Chávez O.³

Affiliation:

1. Researcher, Sección de Estudios de Posgrado e Investigación-Escuela Superior de Ingeniería Mecánica y Eléctrica Ticomán Instituto Politécnico Nacional, Ticomán 600, San Jose Ticoman, Gustavo A. Madero, 07340 Mexico City, Mexico. ORCID: .

2. Coordinator of the Master of Science in Aerospace Engineering Program, Sección de Estudios de Posgrado e Investigación-Escuela Superior de Ingeniería Mecánica y Eléctrica Ticomán Instituto Politécnico Nacional, Ticomán 600, San Jose Ticoman, Gustavo A. Madero, 07340 Mexico City, Mexico.

3. Researcher, Sección de Estudios de Posgrado e Investigación-Escuela Superior de Ingeniería Mecánica y Eléctrica Ticomán Instituto Politécnico Nacional, Ticomán 600, San Jose Ticoman, Gustavo A. Madero, 07340 Mexico City, Mexico (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001185

Reference19 articles.

1. Computational and experimental analysis of flow structures induced by a plasma actuator with burst modulations in quiescent air

2. Corke T. and M. Post. 2005. “Overview of plasma flow control: Concepts optimization and applications.” In Proc. 43rd AIAA Aerospace Sciences Meeting and Exhibit 563. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-563.

3. Numerical investigation of plasma-actuator force-term estimations from flow experiments

4. Plasma Volumetric Effects on the Force Production of a Plasma Actuator

5. High-performance computing-based exploration of flow control with micro devices

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