SBIR/STTR Research Award

3-D Imaging and Fluorescence for Quantification of Liquid and Vapor in Fuel Sprays

Award identifier 3e3199b5b6905eb167adfec6511f9c3abd5fdd8cb341a0a9b5427a95ff7c18c2Awarding agency Department of Defense · Air Force

Award amount

$99,947

Program and phase

SBIR · Phase I

Award year

2011

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
CREARE LLC
Proposal award date
2011-02-18
Contract end date
Not reported
UEI
JDKYAKDT4TT6
Solicitation number
2010.3
Topic code
AF103-196

Research abstract

ABSTRACT: The performance of modern propulsion devices such as gas turbine main combustors and augmentors is largely dependent on fuel spray dynamics. Fuel sprays, usually involving a liquid jet emanating into a gaseous flow followed by subsequent breakup and atomization, are critically important to many performance metrics including thrust, efficiency, static stability, dynamic stability, observability, and emissions. Despite the importance of jet breakup and atomization, these processes are poorly understood and design approaches are largely based on correlations, yielding limited predictive accuracy. The ability to study fuel spray dynamics is limited by existing diagnostics which have difficulty penetrating the dense core region and discriminating between liquid and vapor fuel. In the proposed effort, Creare and the Massachusetts Institute of Technology (MIT) will investigate applying an emerging 3-D flow visualization technique to this problem called Wave Front Imaging (WFI). Laser-Induced Fluorescence (LIF) will be used in combination with WFI (WFI-LIF) to quantify liquid and vapor fuel below the imaging resolution of WFI. In Phase I, we will conduct proof-of-concept experiments using isolated fuel drops vaporizing in hot air. We will compare WFI-LIF with numerical simulations of the same configuration. In Phase II, we will further enhance and calibrate WFI-LIF and extend it to representative flow conditions. BENEFIT: Technology derived from this project will be in the form of a new and novel flow visualization technique to study spray atomization. This will provide new insights into the spray breakup and mixing process, ultimately leading to decreased development time and cost for future propulsion systems while improving performance. This technology will be relevant to a broad range of combustion applications beyond augmentors including military and commercial aircraft combustors and internal combustion engines.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

1,365 SBIR/STTR records share this UEI (1983–2026). Reported award amounts total $507,020,394. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Health and Human Services, Department of Energy, Department of Transportation, Department of Commerce

Agency intelligence

Department of Defense

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