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An insight into the complex phenomena of a turbulent jet diffusion flame, as captured in an image taken at the university of colorado at boulder. The experimental setup, the use of wd-40 as fuel, and the process of flame stabilization against a cement wall. It also discusses the importance of flame stabilization in various devices and engines, and provides some technical details about the image, such as camera settings and photoshop processing.
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Flow Visualization 12/5/
The purpose of this image is to photograph the complex phenomena of a turbulent jet flame. An aerosol can of WD-40 was used as the fuel for the jet diffusion flame. The source of oxidizer for this combustion process is just the oxygen contained in the ambient air. The flame is impinging on a wall as seen below in Figure 1. The fuel jet was shot through a match to ignite the fuel and begin combustion. The only source of light for this image is the small amount of moonlight coming in through the open garage door. The very dark garage enhances the image because of the drastic contrast. For safety reasons, the flame is impinging on a cool cement wall in the garage. Furthermore, the image was taken at night so the garage door could be open to allow for proper ventilation.
Figure 1. Jet Diffusion Flame, Re = 8323.
The general flow set up is shown below in Figure 2. This is a top view of the experimental set-up. The WD-40 aerosol can was approximately two and a half to three feet away from the wall. Initially, the fuel jet was shot through a match to initiate combustion, after which the flame was stabilized near the wall. The camera was approximately two and a half feet away from the flame, next to the wall, as seen in Figure
Flow Visualization 12/5/
μ Re =ρ^ ⋅ v^ ⋅ D Equation 1. Reynold's Number
Where ρ is the density, and after a unit conversion the value for the density of 2- Butoxyethanol is 901.9 kg/m^3. Similarly, after unit conversion, the value for velocity v , characteristic dimension D , and the viscosity μ come out to be 0.703 m/s, 0.0381 m, and 0.0029 kg/m*s respectively. The turbulent jet diffusion flame in Figure 1 was able to be stabilized against a cement wall. Flame stabilization is a very important parameter in combustion, and the design of a combustor. Some examples of common everyday devices that rely on flame stabilization include a furnace, natural gas stove, and a jet aircraft engine. Furthermore, flame stabilization is paramount in the new NASA SCRAMJET engine that traveled at nearly Mach 9.8. Basically, “the attachment of a diffusion flame to a solid or liquid surface is of both fundamental and practical importance because of their relation to flame holding by bodies in combustion chambers” [4]. Flame stabilization, or attachment is theorized to occur when the local velocity of the fluid flow is less than the flame speed. A common feature in flames is a flame base, or edge flame, which attaches to a surface and displays a small dark space in between the flame and the surface. Takahashi et al found that the highest reactivity spot, called the reaction kernel, is formed in a relatively low (<1600K), fuel lean zone of the flame base [4]. Furthermore, the geometric irregularity of the flame base allows for the back-diffusion of radical species, like OH, against the incoming oxidizing stream. The photograph in Figure 1 is not of sufficient quality to show the details of the flame base. But, the stationary reaction kernel located in the flame base “provides a continuous ignition source and sustained stable combustion fast enough to consume the incoming reactants” [4]. Thus, flame stabilization displays a flame base that contains a reaction kernel, and although Figure 1 does not contain sufficient detail to highlight the flame base or reaction kernel, one must exist for flame stabilization.
Figure 2. Experimental Set-up
Below is a list of some parameters that give a little more insight into the photograph.