Mixing Characteristics of Active Microjet-Based Actuators in a Supersonic Backward-Facing-Step Flow-Reference-Cited by-同舟云学术

Mixing Characteristics of Active Microjet-Based Actuators in a Supersonic Backward-Facing-Step Flow

Published:2014-12 Issue:12 Volume:52 Page:2855-2866
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Ahmed Kareem A.¹,Ali Mohd Y.²,Alvi Farrukh S.²

Affiliation:

1. Propulsion and Energy Research Laboratory, Department of Mechanical and Aerospace Engineering, Old Dominion University, Norfolk, Virginia 23529

2. Florida Center for Advanced Aero-Propulsion, Department of Mechanical Engineering, Florida A&M University and Florida State University, Tallahassee, Florida 32310

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053004

Reference37 articles.

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2. Mixing-Controlled Supersonic Combustion

3. Historical Survey on Enhanced Mixing in Scramjet Engines

4. DrummondJ.HamptonV. “Enhancement of Mixing and Reaction in High-Speed Combustor Flowfields,” Vol. 12, NASA Langley Research Center, Technical Rept. 1997, pp. 1–15.

5. Mixing Enhancement in Supersonic Free Shear Flows

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