Numerical Investigation of Transitional Supersonic Base Flows with Flow Control
Author:
Affiliation:
1. University of Arizona, Tucson, Arizona 85721
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.28673
Reference20 articles.
1. Measurement of in-flight base pressure on an artillery-fired projectile
2. Instability Mechanisms in Supersonic Base Flows
3. Numerical investigation of transitional supersonic axisymmetric wakes
4. Direct Numerical Simulations of Transitional Supersonic Base Flows
5. Investigation of Supersonic Wakes Using Conventional and Hybrid Turbulence Models
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