Sphere Drag Coefficients for a Broad Range of Mach and Reynolds Numbers
Author:
Affiliation:
1. ARO Inc., Arnold Air Force Station, Tenn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50387
Reference3 articles.
1. Some experimental results on sphere and disk drag
2. Recent Advances in Gas-Particle Nozzle Flows
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