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A simple finite difference procedure for the vortex controlled diffuserA 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
Document ID
19820034253
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Busnaina, A. A.
(Oklahoma State Univ. Stillwater, OK, United States)
Lilley, D. G.
(Oklahoma State University Stillwater, OK, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 82-0109
Report Number: AIAA PAPER 82-0109
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Orlando, FL
Start Date: January 11, 1982
End Date: January 14, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A17788
Funding Number(s)
CONTRACT_GRANT: NAG3-74
Distribution Limits
Public
Copyright
Other

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