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بررسی جریان درون انژکتورهای فشاری - چرخشی
کبریایی، آزاده Kebriaee, Azadeh
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بررسی جریان درون انژکتورهای فشاری - چرخشی
پدیدآور اصلی :
کبریایی، آزاده Kebriaee, Azadeh
ناشر :
صنعتی شریف
سال انتشار :
1390
موضوع ها :
روش مکان هندسی Level Set Method سوخت پاش های فشاری - چرخشی Pressure-Swirl Injectors مدل...
شماره راهنما :
08-43074
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Thesis
(1)
Pressure Loss of Turbulence Swirling Flow in Convergent Nozzles
(203)
ISME2010-3101
(203)
Pressure Loss of Turbulence Swirling Flow in Convergent Nozzles
(203)
A. N. Broujerdi
(203)
A. Kebriaee
(203)
In this work, pressure loss is simulated analytically in a convergent nozzle. The inlet vector velocity has two components in axial and tangential directions. The governing equations of the turbulence flow are solved by integration method to obtain pressure loss along the nozzle wall.The results show that the boundary layer thickness depends only on the nozzle angles, Reynolds number and Roseby number. It is also found that pressure distribution decreases drastically near the outlet of the nozzle about 100 percent in average in different conditions. The maximum value of the boundary layer thickness is about three times of the outlet thickness.
(203)
turbulent swirling flow, boundary layer, integration method
(203)
Instability Investigation of Taylor-Couette Flow with an Axial Velocity
(209)
Simulation of turbulent swirling flow in convergent nozzles
(213)
Upwind Compact and Explicit High Order Finite Difference Scheme for Level Set Technique
(221)
Numerical Simulation of Laminar and Turbulent Two-Phase Flow in Pressure-Swirl Atomizers
(247)
Spiral Viscous Flow Stability between Coaxial Cylinders by
(277)