Sub-Boundary-Layer Disturbance Effects on Supersonic Base-Pressure Fluctuations
Author:
Affiliation:
1. ATK-Thiokol Propulsion, Promontory, Utah 84307
2. University of Texas at Arlington, Arlington,Texas 76019
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.12769
Reference14 articles.
1. Supersonic base flow experiments in the near wake of a cylindrical afterbody
2. Investigation of large-scale structures in supersonic planar base flows
3. Measurement of inflight base-pressure on an artillery-fired projectile
4. Effects of vortex generators on the growth of a compressible shear layer
5. Effect of tabs on the flow and noise field of an axisymmetric jet
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