SBIR/STTR Research Award

Physical Sub-Model Development for Turbulence Combustion Closure

Award identifier 275ff5246b9dc04196bb8ab78d0661cd1f93589eb7cb244faba8c6c3b45334d9Awarding agency Department of Defense · Air Force

Award amount

$149,996

Program and phase

STTR · Phase I

Award year

2014

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
Proposal award date
2014-05-15
Contract end date
2014-10-14
UEI
XGYZK5MHNJZ8
Solicitation number
2013.
Topic code
AF13-AT12

Research abstract

ABSTRACT: The innovation proposed is a computationally-tractable, physics-based, portable turbulent combustion modeling strategy for application to a wide range of Air Force aero-propulsive systems, including augmentors, liquid rockets and scramjets. This modeling strategy will be implemented within an Application Programming Interface (API) library suitable for easy integration within Air Force CFD simulation codes. The significance of the innovation is that it will improve the predictive capabilities of these codes with regard to the interaction of highly-unsteady, turbulent flows with combustion processes. As a result, CFD simulations will be able to capture more accurately and in a cost effective manner the complex flow physics governing propulsion system performance and stability. This combustion model library will involve a multi-layered approach that includes a range of formulations applicable to different flame regimes and with varying degrees of computational costs. By providing a viable and accurate modeling strategy of lasting relevance applicable for routine analysis, the appropriate model may be chosen for a particular problem/scenario while minimizing computational cost. BENEFIT: In order to ensure portability and easy coupling with appropriate reacting CFD flow solvers, the proposed modeling strategy will be implemented within a portable library featuring a standardized multi-language Application Programming Interface (API). This API library represents a viable commercial product to be licensed to customers who require access to advanced turbulent combustion models in their CFD flow solver of choice. Combustion models available in the API library will be applicable to a wide range of military and commercial combustion applications, including gas turbines, augmentors, power generation systems, furnaces, incinerators, internal combustion engines, etc. The commercial opportunities for this standardized API library are enormous. CRAFT Tech will market this library for license to commercial customers as well as to other CFD flow solver development companies.

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

303 SBIR/STTR records share this UEI (1995–2025). Reported award amounts total $121,181,328. 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, National Science Foundation

Agency intelligence

Department of Defense

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