SBIR/STTR Research Award

Compact Kinetic Mechanisms for Petroleum-Derived and Alternative Aviation Fuels

Award identifier 885058572841b3f2a1b58eb7d5f32e5155217bf4abec5a7efa827610e43fdcbdAwarding agency National Aeronautics and Space Administration

Award amount

$124,837

Program and phase

SBIR · Phase I

Award year

2014

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
SPECTRAL ENERGIES LLC
Proposal award date
2014-06-20
Contract end date
2014-12-19
UEI
C3DAVH4VJDG3
Solicitation number
Not reported
Topic code
A3.03

Research abstract

To be useful for computational combustor design and analysis using tools like the National Combustion Code (NCC), low-dimensional chemical kinetic mechanisms for modeling of real fuel combustion chemistry must be sufficiently compact so that they can be utilized in multi-dimensional, multi-physics, reacting computational fluid dynamics (CFD) simulations. Despite advances in CFD-appropriate kinetic mechanism reduction for kerosene-range fuels, significant combustion property variation among current and prospective certified fuels remains a challenge for meaningful CFD-advised design of high pressure, low-emissions combustors. The proposed project will leverage Princeton's ongoing work in aviation fuel surrogate formulation and modeling as well as kinetic mechanism development for emissions and high pressure combustion to produce and demonstrate a meta-model framework for automated generation of fuel-flexible compact chemical kinetic mechanisms appropriate for 3-D combustion CFD codes. Phase I will demonstrate the novel meta-model approach by providing compact kinetic mechanisms for both a "typical" Jet A/JP-8 (POSF-4658), as well as a synthetic paraffinic kerosene (SPK) derived from natural gas (POSF 4734). Phase II of this proposed work would generalize the Phase I results to span the combustion property parameter space relevant to both conventional and next-generation alternative aviation fuels. The commercial product foreseen from this SBIR program is a stand-alone, novice-friendly real fuel kinetic mechanism generator software package that can interface with commercially-available computational fluid dynamics (CFD) codes. Potential customers may include the companies supplying ANSYS, CFD-ACE+, or COMSOL, as well as industrial users with proprietary in-house codes. Tools to yield compact real fuel kinetic models has similar broad appeal for computational simulations in automotive, aerospace (both defense and civilian), and marine propulsion industries.

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

272 SBIR/STTR records share this UEI (2007–2026). Reported award amounts total $120,780,215. 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 Energy, Department of Health and Human Services, Department of Agriculture

Agency intelligence

National Aeronautics and Space Administration

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