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A fuel nozzle for use in a gas turbine includes a pre-mix flow passage for directing a flow segment of a flow of a working fluid through the fuel nozzle. A first swirler vane and a second swirler vane extend within the pre-mix flow passage. The first swirler vane provides a first wake region within

A fuel nozzle for use in a gas turbine includes a pre-mix flow passage for directing a flow segment of a flow of a working fluid through the fuel nozzle. A first swirler vane and a second swirler vane extend within the pre-mix flow passage. The first swirler vane provides a first wake region within the flow segment. The second swirler vane provides a second wake region within the flow segment. A fuel injection peg is disposed downstream from the first swirler vane and the second swirler vane. The fuel injection peg is positioned within the flow segment between the first wake region and the second wake region.

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1. A fuel nozzle for a combustor, the fuel nozzle comprising: a nozzle body;an outer sleeve circumferentially surrounding at least a portion of the nozzle body, wherein the outer sleeve and the nozzle body define a premix flow passage therebetween;a first swirler vane circumferentially spaced from a

1. A fuel nozzle for a combustor, the fuel nozzle comprising: a nozzle body;an outer sleeve circumferentially surrounding at least a portion of the nozzle body, wherein the outer sleeve and the nozzle body define a premix flow passage therebetween;a first swirler vane circumferentially spaced from a second swirler vane, wherein the first and second swirler vanes extend from the nozzle body to the outer sleeve within the premix flow passage, and a trailing edge of the first and second swirler vanes each form a first angle relative to an axial centerline of the nozzle body;a fuel injection peg having an airfoil shape comprising a leading edge, a trailing edge, a pressure side, and a suction side that extends from the nozzle body to the outer sleeve, wherein the leading edge of the fuel injection peg is positioned downstream from a trailing edge of the first swirler vane and a trialing edge of the second swirler vane within the premix passage, and the trailing edge of each fuel injection peg forming a second angle relative to the axial centerline of the nozzle body that is the same as the first angle; and;a uniform flow region that is formed circumferentially between the first swirler vane and second swirler vane and extends downstream the first and second swirler vanes along a direction of the second angle;wherein the fuel injection peg maintains a radial contour between the nozzle body and outer sleeve that is consistent with a radial contour of the swirler vanes, such that the fuel injection peg is positioned within the uniform flow region, and the leading edge of the fuel injection peg is circumferentially offset from the trailing edge of the first swirler vane and circumferentially offset from the trailing edge of the second swirler vane. 2. The fuel nozzle as in claim 1, wherein the trailing edge of the fuel injection peg is circumferentially offset from the trailing edge of the first swirler vane and circumferentially offset from the trailing edge of the second swirler vane. 3. The fuel nozzle as in claim 1, wherein the fuel injector peg includes at least one fuel injection port. 4. The fuel nozzle as in claim 1, wherein the fuel injector peg includes at least one fuel injection port disposed along the concave pressure side wall. 5. The fuel nozzle as in claim 1, wherein the fuel injector peg includes at least one fuel injection port disposed along the convex suction side wall. 6. A combustor, comprising: a plurality of fuel nozzles radially and circumferentially arranged across an end cover and extending axially downstream from the end cover within an outer casing, at least one fuel nozzle of the plurality of fuel nozzles comprising:a nozzle body;an outer sleeve circumferentially surrounding at least a portion of the nozzle body, wherein the outer sleeve and the nozzle body define a premix flow passage therebetween;a plurality of swirler vanes circumferentially spaced about the nozzle body and extending from the nozzle body to the outer sleeve within the premix flow passage, each swirler vane having a trailing edge that forms a first angle relative to an axial centerline of the nozzle body;a plurality of fuel injection pegs disposed within the premix passage, each fuel injection peg having an airfoil shape comprising a leading edge, a trailing edge, a pressure side and a suction side that extends from the nozzle body to the outer sleeve, wherein the leading edge of each fuel injection peg is positioned downstream from a corresponding pair of circumferentially adjacent trailing edges of circumferentially adjacent swirler vanes of the plurality of swirler vanes, and the trailing edge of each fuel injection peg forming a second angle relative to the axial centerline of the nozzle body that is the same as the first angle; anda uniform flow region that is formed circumferentially between the first swirler vane and second swirler vane and extends downstream the first and second swirler vanes in a direction of the second angle;wherein each of the fuel injection pegs maintains a radial contour between the nozzle body and outer sleeve that is consistent with a radial contour of the corresponding circumferentially adjacent swirler vanes, such that the fuel injection peg is positioned within the uniform flow region, and the leading edge of each fuel injection peg is circumferentially offset from the trailing edges of the corresponding circumferentially adjacent swirler vanes of the plurality of swirler vanes. 7. The combustor as in claim 6, wherein the trailing edge of each fuel injection peg is circumferentially offset from the trailing edges of the corresponding circumferentially adjacent swirler vanes of the plurality of swirler vanes. 8. The combustor as in claim 6, Wherein at least one fuel injector peg of the plurality of fuel injector pegs includes at least one fuel injection port. 9. The combustor as in claim 6, wherein at least one fuel injector peg of the plurality of fuel injector pegs includes at least one fuel injection port disposed along the pressure side wall. 10. The combustor as in claim 6, wherein at least one fuel injector peg of the plurality of the injector pegs includes at least one fuel injection port disposed along the suction side wall.