Modeling of Performance of an Artillery Shell Using Neural Networks
Author:
Affiliation:
1. Indian Institute of Technology Kanpur, Kanpur 208016, UP, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3832
Reference18 articles.
1. Fluctuating Wall Pressure under a Separated Supersonic Flow
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3. Hypersonic flow over axially symmetric spiked bodies
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5. New Diagnostic Technique for the Study of Turbulent Boundary-Layer Separation
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