A comparative study of full Navier-Stokes and Reduced Navier-Stokes analyses for separating flows within a diffusing inlet S-duct
Abstract
A three-dimensional implicit Full Navier-Stokes (FNS) analysis and a 3D Reduced Navier-Stokes (RNS) initial value space marching solution technique has been applied to a class of separate flow problems within a diffusing S-duct configuration characterized as vortex-liftoff. Both Full Navier-Stokes and Reduced Navier-Stokes solution techniques were able to capture the overall flow physics of vortex lift-off, however more consideration must be given to the development of turbulence models for the prediction of the locations of separation and reattachment. This accounts for some of the discrepancies in the prediction of the relevant inlet distortion descriptors, particularly circumferential distortion. The 3D RNS solution technique adequately described the topological structure of flow separation associated with vortex lift-off.
- Publication:
-
Joint Propulsion Conference and Exhibit
- Pub Date:
- June 1993
- Bibcode:
- 1993jpmc.confR..28A
- Keywords:
-
- Computational Fluid Dynamics;
- Ducted Flow;
- Engine Airframe Integration;
- Flow Distortion;
- Inlet Flow;
- Navier-Stokes Equation;
- Separated Flow;
- Pressure Recovery;
- Turbulence Models;
- Vortices;
- Astrodynamics