PNS computations for spinning and fin-stabilized projectiles at supersonic velocities
Author:
Affiliation:
1. U.S. Army, Ballistics Research Laboratories, Aberdeen Proving Ground, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-2118
Reference34 articles.
1. Computations of the Magnus effect for slender bodies in supersonic flow
2. Computational parametric study of the Magnus effect on boattailed shell at supersonic speeds
3. New implicit boundary procedures - Theory and applications
4. Calculation of viscous supersonic flows over finned bodies
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1. Numerical Simulations of Projectile Base Flow;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
2. Navier-Stokes computations of finned kinetic energy projectile base flow;20th Atmospheric Flight Mechanics Conference;1995-08-07
3. Navier-Stokes code verification for projectile configurations at supersonic and transonic velocities;15th Aerodynamic Testing Conference;1988-05-18
4. Viscous calculations of supersonic flows past cylinders at angles ofattack;5th Applied Aerodynamics Conference;1987-08-17
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