Abstract
The Free Form Deformation method was applied to a S-duct geometry to reduce total pressure losses and flow distortion. The deformation method was coupled with a multi-objective genetic algorithm to optimize the shape of a diffusing S-duct, which was previously investigated, both numerically and experimentally. During the optimization process, 200 deformed shapes were tested with steady-state CFD simulations and the performances were evaluated both in terms of total pressure losses and swirl angle at the outlet. It was obtained a Pareto front with a maximum total pressure losses reduction of 20% and a maximum swirl reduction of 10%. The two extreme points of the Pareto front were further investigated by transient Detached Eddy Simulations to assess also the impact of the optimization on the flow instability. Surprisingly, one of the solutions showed stable and stationary vortical structures. This is in strong contrast with the previous investigations of the flow field time history of the baseline configuration, which outlined strong oscillations of the flow field combined with a high increase of the distortion parameters in comparison with the time-averaged flow field.
Original language | English |
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Title of host publication | 23rd AIAA Computational Fluid Dynamics Conference, 2017 |
Publisher | American Institute of Aeronautics and Astronautics Inc. |
ISBN (Print) | 9781624105067 |
Publication status | Published - 2017 |
Event | 23rd AIAA Computational Fluid Dynamics Conference, 2017 - Denver, USA United States Duration: 5 Jun 2017 → 9 Jun 2017 |
Conference
Conference | 23rd AIAA Computational Fluid Dynamics Conference, 2017 |
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Country/Territory | USA United States |
City | Denver |
Period | 5/06/17 → 9/06/17 |
ASJC Scopus subject areas
- Mechanical Engineering
- Energy Engineering and Power Technology
- Fluid Flow and Transfer Processes
- Aerospace Engineering