Investigation of Supersonic Wakes Using Conventional and Hybrid Turbulence Models
Author:
Affiliation:
1. The University of Arizona, Tucson, Arizona 85721
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.20379
Reference32 articles.
1. Measurement of in-flight base pressure on an artillery-fired projectile
2. Supersonic base flow experiments in the near wake of a cylindrical afterbody
3. Planar visualizations of large-scale turbulent structures in axisymmetric supersonic separated flows
4. Supersonic near-wake afterbody boattailing effects on axisymmetric bodies
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1. Aerodynamic drag of axisymmetric models with different boattail angles under subsonic and supersonic flow conditions;Journal of Mechanical Science and Technology;2023-12
2. Flow Structure Identification in the Near Wake of a Supersonic Separated Flow Using FAEMD;2018 Fluid Dynamics Conference;2018-06-24
3. Computational study of supersonic turbulent-separated flows using partially averaged Navier-stokes method;Acta Astronautica;2015-02
4. Numerical investigation of turbulent supersonic axisymmetric wakes;Journal of Fluid Mechanics;2012-06-07
5. Identification of large coherent structures in supersonic axisymmetric wakes;Computers & Fluids;2009-09
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