Large eddy simulation of supersonic base flow
Author:
Affiliation:
1. Defence Research Establishment, Stockholm, Sweden
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-426
Reference11 articles.
1. [l] Rollstin L.; 1987, "Measurement of Inflight BasePressure~onanArtillery-Fired Projectile", AIAA PaperNo. 87-2427.
2. Optimization of Drag Minimums Including Effects of Flow Separation
3. Agrell J. & White R.A.; 1974, "An Experimental Investigation of Supersonic Axisymmetric Flow over Boattails Containing aCentered Propulsive Jet", FFA, TN AU-913.
4. Supersonic near-wake afterbody boattailing effects on axisymmetric bodies
5. Cylindrical afterbodies in supersonic flow with gas ejection.
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