NASA NTRS · 19820034253
A simple finite difference procedure for the vortex controlled diffuser
Abstract
A simple prediction procedure for sudden expansion incompressible flows is developed and applied to the vortex controlled diffuser. Transient Navier-Stokes equations of an incompressible fluid are solved by means of their associated finite difference equations in terms of the primitive pressure velocity variables. A computer code is developed using a laminar flow simulation with free slip or no slip wall boundary conditions. In addition, predicted results confirm that effectiveness increases with increases in duct length and bleed flow rate
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Busnaina, A. A., Lilley, D. G.. 1982-01-01. A simple finite difference procedure for the vortex controlled diffuser. https://ntrs.nasa.gov/citations/19820034253
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