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Research Article

Effect of Flow Parameters and Injection Flow Area on Non-Premixed Methane/Oxygen Diffusion Flame Stability

, , , &
Pages 539-557 | Received 15 Jan 2020, Accepted 20 May 2020, Published online: 07 Jun 2020
 

ABSTRACT

The focus of this research was the design, fabrication, and testing of an experimental non-premixed flame burner to determine the effect of gaseous flow parameters and flow geometry on the stability of methane/oxygen combustion. The non-premixed burner consisted of a horizontally mounted, rectangular combustion chamber with a single coaxial injector, capable of introducing reactants at a specified impingement angle of 30° at the exit plane. Gaseous oxygen was the primary flow and gaseous methane was the secondary flow. The non-premixed burner was equipped with optical windows on both sides of the chamber parallel to the axis of the flame, which allowed for clear viewing of the product flame. Ignition of the reactants was achieved by a retractable spark plug. Stability maps of the resultant diffusion flame were created for three different injection flow areas based upon reactant equivalence ratio and primary reactant Reynolds numbers. The results showed that decreasing the primary flow area resulted in a more stable flame condition over a broader range of Reynolds numbers (laminar flow to over 40000) and equivalence ratios (fuel-lean 0.27 to fuel-rich 4.94). Increasing Reynolds number also resulted in a transition from a stable, anchored flame to a detached, unstable flame.

Nomenclature

CRES=

Corrosion resistant stainless-steel

D=

Diameter of flow, mm

GCH4=

Gaseous methane

GH2=

Gaseous hydrogen

GN2=

Gaseous nitrogen

GO2=

Gaseous oxygen

L=

Length, mm

(O/F)=

Oxidizer-to-fuel ratio

P=

Pressure, kPa

Pox=

partial oxidation

Re=

Reynolds number

V=

Velocity, m/s

XSTO=

Non-dimensional average flame standoff distance

Greek Symbols=
Φ=

Equivalence ratio

Subscripts=
Annular=

Annular region of coaxial injector

CH4=

Methane

D=

Diameter

H=

Hydraulic

Mass=

Mass

Mole=

Mole

Mom=

Momentum

O2=

Oxygen

SD=

Standoff distance

Acknowledgments

The authors wish to thank the Penn State Altoona Research and Sponsored Programs office and Mr. Corey Griffin for sponsoring this internal research grant. Thanks to Mr. Morgan Litzinger, Mr. Lucas Nunamaker, and Mr. Jordan Crist for design, fabrication, and initial checkout testing of the experimental diffusion burner chamber. Special thanks to Mr. Tom Hatch for machining of the spark plug igniter pneumatic cylinder mounting bracket, Mr. Dillon Over for assistance with upstream flow manifold assembly, Mr. Joshua Hollingshead for assembly work, machining, test assistance, and welding of the experimental cart, and Mr. Sydney Damgaard for assistance in video cinematography data review.

Additional information

Funding

This work was supported by internal funding from Penn State Altoona.

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