NUMERICAL INVESTIGATION OF A STEADY NONEVAPORATING HOLLOW-CONE SPRAY INTERACTING WITH AN ANNULAR AIR JET

2001 ◽  
Vol 11 (2) ◽  
pp. 14 ◽  
Author(s):  
Woo Tae Kim ◽  
Kang Y. Huh ◽  
Jacob A. Friedman ◽  
Metin Renksizbulut
Keyword(s):  
Numerical Investigation ◽  
Hollow Cone ◽  
Air Jet ◽  
Hollow Cone Spray

Characteristics of Leeward Shear Layer Structure of Hollow-Cone Spray in Gaseous Crossflow

AIAA Journal ◽  
2021 ◽  
Vol 59 (1) ◽  
pp. 405-409
Author(s):  
Haibin Zhang ◽  
Shilin Gao ◽  
Bofeng Bai ◽  
Yechun Wang
Keyword(s):  
Shear Layer ◽  
Layer Structure ◽  
Hollow Cone ◽  
Hollow Cone Spray

scholarly journals Spray Drop Size and Velocity Measurements in a Swirl-Stabilized Combustor

1991 ◽  
Author(s):  
B. Chehroudi ◽  
M. Ghaffarpour
Keyword(s):  
Drop Size ◽  
Cone Angle ◽  
Hollow Cone ◽  
Flow Rates ◽  
Fuel Droplets ◽  
Radial Profiles ◽  
Fuel Nozzle ◽  
Pass Through ◽  
Yellow Region ◽  
Hollow Cone Spray

A pressure-swirl fuel nozzle generating a hollow-cone spray with nominal cone angle of 30 degrees is used in a swirl-stabilized combustor. The combustor is circular in cross section with swirl plate and fuel nozzle axes aligned and coinciding with the axis of the chamber. Kerosene is injected upward inside the chamber from the fuel nozzle. Separate swirl and dilution air flows are uniformly distributed into the chamber that pass through the honey comb flow straighteners and screens. Calculated swirl number of 1.5 is generated with the design swirl plate exit air velocity of 30 degrees with respect to the chamber axis. Effects of swirl and dilution air flow rates on the shape and stability of the flame are investigated. Stable and classical liquid fuel sheet disintegration zone exists close to the nozzle with no visible light followed by a luminous blue region and a mixed blue/yellow region that subsequently turns into yellow for most of the part in the flame. A Phase Doppler Particle Analyzer (PDPA) is used to measure drop size, mean and rms axial velocity for two cases of with and without combustion at six different axial locations from the nozzle. For the no-combustion case all air and fuel flow rates were kept at the same values as the combusting spray condition. Results for mean axial drop velocity profiles indicate widening of the spray due to combustion while the magnitudes of the peak velocities are slightly increased. No measurements inside the hollow-cone spray are possible due to burning of fuel droplets. Drop turbulence decreases due to combination of increase in gas kinematic viscosity and elimination of small drops at high temperatures. Sauter Mean Diameter (SMD) radial profiles at all axial locations increase with combustion due to preferential burning of small drops.

Analysis of a Prototype High-Pressure “Hollow Cone Spray” Diesel Injector Performance in Optical and Metal Research Engines

2017 ◽  
Author(s):  
Carlo Beatrice ◽  
Giacomo Belgiorno ◽  
Gabriele Di Blasio ◽  
Ezio Mancaruso ◽  
Luigi Sequino ◽  
...  
Keyword(s):  
High Pressure ◽  
Hollow Cone ◽  
Metal Research ◽  
Hollow Cone Spray

Validation of a CFD Model of a Hollow-Cone Spray with Gasoline Fuel Blends

2011 ◽  
Author(s):  
Lars Schmidt ◽  
Jason King ◽  
John Stokes ◽  
James Mullineux ◽  
Calvin R.Ramasamy ◽  
...  
Keyword(s):  
Cfd Model ◽  
Hollow Cone ◽  
Fuel Blends ◽  
Hollow Cone Spray

Numerical Investigation on Visualizations of Confined Air Flow in a Slot Jet Inside a Rectangular Channel

2015 ◽  
Vol 813-814 ◽  
pp. 736-741
Author(s):  
M. Muthukannan ◽  
P. Rajesh Kanna ◽  
S. Jeyakumar ◽  
J.Y. Raja Shangaravel ◽  
S. Raghu ◽  
...  
Keyword(s):  
Reynolds Number ◽  
Flow Field ◽  
Numerical Investigation ◽  
Rectangular Channel ◽  
Reynolds Numbers ◽  
Vortex Center ◽  
Computational Domain ◽  
Reattachment Length ◽  
Aspect Ratios ◽  
Air Jet

In the present numerical investigation, the flow field of confined slot air jet in a rectangular computational domain is reported. In the present work the flow field parameters like reattachment length, vortex center and horizontal velocity profiles for various Reynolds numbers and for various aspect ratios are presented .The present study reveals that the vortex centers are moving in a downstream direction with increase in Reynolds number. The reattachment length is directly dependent on the Reynolds numbers. In case of vortex dynamics, the vortex size is indirectly dependent on the inlet jet width. In the present investigation, SIMPLE algorithm is used to solve the governing equations. It is concluded that the aspect ratio and the Reynolds number are playing dominant roles in flow field of the present computational domain.

Mixing of Hollow-Cone Spray with a Confined Crossflow in Rectangular Duct

AIAA Journal ◽  
2013 ◽  
Vol 51 (3) ◽  
pp. 615-622 ◽  
Author(s):  
Haibin Zhang ◽  
Bofeng Bai ◽  
Li Liu ◽  
Huijuan Sun ◽  
Junjie Yan
Keyword(s):  
Rectangular Duct ◽  
Hollow Cone ◽  
Hollow Cone Spray
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