Supersonic base flow experiments in the near wake of a cylindrical afterbody
Author:
Affiliation:
1. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11953
Reference18 articles.
1. Turbulent flow predictions for afterbody/nozzle geometries includingbase effects
2. Supersonic flow over cylindrical afterbodies with base bleed
3. Subsonic/transonic prediction capabilities for nozzle/afterbody configurations
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