Effectiveness of passive devices for axisymmetric base drag reduction at Mach 2
Author:
Affiliation:
1. National Aeronautical Laboratory, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26130
Reference6 articles.
1. Reduction of base drag
2. Passive devices for axisymmetric base drag reduction at transonic speeds
3. Effect of Base Cavities on the Aerodynamic Drag of an Axisymmetric Cylinder
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