Navier-Stokes Analysis of Subsonic Flowfields over a Missile Configuration
Author:
Affiliation:
1. U.S. Naval Postgraduate School, Monterey, California 93943
2. U.S. Naval Air Warfare Center, China Lake, California 93555
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3318
Reference11 articles.
1. High Angle of Attack Aerodynamics
2. Computation of turbulent supersonic flows around pointed bodies having crossflow separation
3. Numerical simulation of vortex unsteadiness on slender bodies of revolution at large incidence
4. Analysis of flowfields over missile configurations at subsonic speeds
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2. Aerodynamic shape optimization of guided missile based on wind tunnel testing and computational fluid dynamics simulation;Thermal Science;2017
3. Missile Aerodynamics;Encyclopedia of Aerospace Engineering;2010-12-15
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