Three-Dimensional Structure of the Compressible Mixing Layer of an Axisymmetric, Supersonic, Separated Flow
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3084
Reference33 articles.
1. Measurement of inflight base-pressure on an artillery-fired projectile
2. Reedy, T. M. “Control of Supersonic Axisymmetric Base Flows Using Passive Splitter Plates and Pulsed Plasma Actuators,” Ph.D. Dissertation,Department of Mechanical Science and Engineering, Universityof Illinois at Urbana-Champaign, IL,2013.
3. DeBlauw, B. G. “Active Control of Massively Separated High-Speed/Base Flows with Electric Arc Plasma Actuators,” Ph.D. Dissertation,Department of Aerospace Engineering, Universityof Illinois at Urbana-Champaign, IL,2012.
4. Supersonic near-wake afterbody boattailing effects on axisymmetric bodies
5. Velocity and turbulence measurements in a supersonic base flow with mass bleed
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1. Planar and Volumetric Turbulent Mode Dynamics of a Supersonic Separated/Reattaching Flow;AIAA Aviation 2019 Forum;2019-06-15
2. Three-Dimensional Entrainment Dynamics of a Supersonic Base Flow;AIAA Scitech 2019 Forum;2019-01-06
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