Experimental Investigation of Flow Control on a High-Lift Wing Using Modulated Pulse Jet Vortex Generator-Reference-Cited by-同舟云学术

Experimental Investigation of Flow Control on a High-Lift Wing Using Modulated Pulse Jet Vortex Generator

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:

Abdolahipour Soheila¹,Mani Mahmoud²^ORCID,Shams Taleghani Arash³^ORCID

Affiliation:

1. Ph.D., Aerospace Research Institute, Ministry of Science, Research, and Technology, Mahestan St., Shahrak-e-gharb, P.O. Box 14665-834, Tehran 1465774111, Iran.

2. Professor, Dept. of Aerospace Engineering, Amirkabir Univ. of Technology, No. 350, Hafez Ave., Valiasr Square, Tehran 1591634311, Iran. ORCID: .

3. Assistant Professor, Aerospace Research Institute, Ministry of Science, Research, and Technology, Mahestan St., Shahrak-e-gharb, P.O. Box 14665-834, Tehran 1465774111, Iran (corresponding author). ORCID: .

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.1943-5525.0001463

Reference61 articles.

1. Parametric study of a frequency-modulated pulse jet by measurements of flow characteristics

2. Aley K. T. K. Guha and R. Kumar. 2018. “Experimental characterization of a high-lift supercritical airfoil with microjets.” In Proc. 2018 Flow Control Conf. 3688. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3688.

3. Active Flow Control of a High-Lift Supercritical Airfoil with Microjet Actuators

4. Controlled transients of flow reattachment over stalled airfoils

5. Role of Actuation Frequency in Controlled Flow Reattachment over a Stalled Airfoil

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