Passive devices for axisymmetric base drag reduction at transonic speeds
Author:
Affiliation:
1. National Aeronautical Laboratory, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45586
Reference4 articles.
1. Reduction of base drag
2. Subsonic axisymmetric base flow experiments with base modifications
3. Effect of Base Cavities on the Aerodynamic Drag of an Axisymmetric Cylinder
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