Microvortex Generator Controlled Shock–Boundary Layer Interactions in Hypersonic Intake-Reference-Cited by-同舟云学术

Microvortex Generator Controlled Shock–Boundary Layer Interactions in Hypersonic Intake

Published:2021-03 Issue:2 Volume:34 Page:04020120
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jana Tamal¹,T. Thillaikumar¹,Kaushik Mrinal²^ORCID

Affiliation:

1. Ph.D. Candidate, Dept. of Aerospace Engineering, Indian Institute of Technology Kharagpur, Kharagpur, West Bengal 721302, India.

2. Associate Professor, Dept. of Aerospace Engineering, Indian Institute of Technology Kharagpur, Kharagpur, West Bengal 721302, India (corresponding author). ORCID: .

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.1943-5525.0001239

Reference33 articles.

1. Anderson B. J. Tinapple and L. Surber. 2006. “Optimal control of shock wave turbulent boundary layer interactions using micro-array actuation.” In Proc. 3rd AIAA Flow Control Conf. Washington DC: American Institute of Aeronautics and Astronautics.

2. Ashill P. J. Fulker and K. Hackett. 2001. “Research at DERA on sub boundary layer vortex generators (SBVGs).” In Proc. 39th Aerospace Sciences Meeting and Exhibit. Washington DC: American Institute of Aeronautics and Astronautics.

3. Shock Wave–Boundary-Layer Interactions

4. Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions

5. Subsonic diffusers designed integrally with vortex generators.

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