DocumentCode
3356203
Title
Numerical Simulation on the Flow Fields Downstream Nozzles with Tabs by Modified Turbulent Model
Author
Zhang, Yufang ; Wang, Fang ; Huang, Yong ; Li, Jingxuan
Author_Institution
Dept. of Thermal Power Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing
fYear
2009
fDate
27-31 March 2009
Firstpage
1
Lastpage
4
Abstract
Firstly, the flow fields downstream one axisymmetric nozzles and a nozzle with four tabs were simulated with four different turbulent models, and the results were compared with experimental data. Then the flow fields downstream nozzles with tabs of varied orientation angles were predicted for different orientation angles of the tabs while the projected blockage of tabs was kept unchanged. The predictions were also compared with that of the nozzle without tabs. The decrease of potential core length was remarkable when tabs were affixed. As the orientation angle increased, the potential core length decreased firstly and then increased. The streamwise vortices strength increased straightly with the orientation angle. Both entrainment gain and thrust losses of the nozzles decreased as the orientation angle increased.
Keywords
flow simulation; nozzles; turbulence; entrainment gain; flow fields downstream nozzles; streamwise vortices strength; thrust losses; turbulent model; Aerodynamics; Boundary conditions; Equations; Fluctuations; Laboratories; Numerical simulation; Power engineering; Predictive models; Temperature; Thermal engineering;
fLanguage
English
Publisher
ieee
Conference_Titel
Power and Energy Engineering Conference, 2009. APPEEC 2009. Asia-Pacific
Conference_Location
Wuhan
Print_ISBN
978-1-4244-2486-3
Electronic_ISBN
978-1-4244-2487-0
Type
conf
DOI
10.1109/APPEEC.2009.4918547
Filename
4918547
Link To Document