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Amy Lynch

Researcher at Air Force Research Laboratory

Publications -  37
Citations -  625

Amy Lynch is an academic researcher from Air Force Research Laboratory. The author has contributed to research in topics: Combustor & Combustion. The author has an hindex of 12, co-authored 37 publications receiving 577 citations. Previous affiliations of Amy Lynch include University of Dayton Research Institute & Wright-Patterson Air Force Base.

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Emissions Characteristics of a Turbine Engine and Research Combustor Burning a Fischer−Tropsch Jet Fuel

TL;DR: In this paper, the emissions characteristics of two combustion platforms, a T63 turboshaft engine and an atmospheric swirl-stabilized research combustor, fueled with conventional military jet fuel (JP-8), a natural-gas-derived Fischer−Tropsch synthetic jet fuel, and blends of the two were investigated.
Journal ArticleDOI

Flame and Flow Topologies in an Annular Swirling Flow

TL;DR: In this article, the authors investigate flame shapes and flow configurations in a premixed, swirl-stabilized dump combustor and present results from high-speed luminosity imaging, particle image velocimetry (PIV), and OH-planar laser induced fluorescence (PLIF) to illustrate time-averaged and instantaneous flame shape and flow fields associated with the different configuration families.
Proceedings ArticleDOI

A Detailed Investigation of Bluff Body Stabilized Flames

TL;DR: In this paper, it is concluded that the vortex dynamics and not geometry is the dominant mechanism for blimp body flame extinction and this conclusion is supported by the lean blowout data, by the high speed images and reference data from NACA.

A detailed investigation of bluff body stabilized flames (postprint)

TL;DR: In this paper, it was concluded that the vortex dynamics and not geometry is the dominant mechanism for bluff body flame extinction, and this conclusion was supported by the lean blowout data, by the high speed images and reference data from NACA.
Journal ArticleDOI

Characterization of flame-shedding behavior behind a bluff-body using proper orthogonal decomposition

TL;DR: In this paper, the authors quantitatively identify the contribution of various instability modes for three 1.5-in. flameholder configurations and is performed in an augmentor test rig employing propane and air as fuel and oxidizer, respectively.