Three-Component Turbulence Measurements and Analysis of a Supersonic, Axisymmetric Base Flow
Author:
Affiliation:
1. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801
Funder
Army Research Office
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057859
Reference37 articles.
1. Numerical Computations of Supersonic Base Flow with Special Emphasis on Turbulence Modeling
2. Three-dimensional flow calculations for a projectile with standard and dome bases
3. Application of the RNG turbulence model to the simulation of axisymmetric supersonic separated base flows
4. Measurement of inflight base-pressure on an artillery-fired projectile
5. Large eddy simulation of supersonic base flow
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