Computational Fluid Dynamics of Liquid Filled Spinning Shells.
Final rept. 25 May 82-25 May 83,
STANFORD UNIV CA DEPT OF AERONAUTICS AND ASTRONAUTICS
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A fully implicit, three-dimensional finite difference simulation of the incompressible Navier-Stokes equations has been cast using upwind operators. A non-inertial coordinate system was used to simulate the fluid motion in a processing and spinning cylinder. The continuity equation was modified to include artificial compressibility. The code is capable of time accurate solutions, and it could be used to track time-dependent flows. Keywords Incompressible flow Finite difference methods Navier-Stokes equations Liquid-filled projectile.
- Fluid Mechanics