SBIR/STTR Research Award

An Enhanced Software Toolkit for OpenNCC to Reduce NOx in Commercial Supersonic Transport Combustors

Award identifier fa566e9212be322721ebc8b36d54741901a1803f99b620d4626c13367c545ae4Awarding agency National Aeronautics and Space Administration

Award amount

$124,999

Program and phase

SBIR · Phase I

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
Proposal award date
2019-08-19
Contract end date
2020-02-18
UEI
XGYZK5MHNJZ8
Solicitation number
SBIR_19_P1
Topic code
A1

Research abstract

The innovation proposed is a second-generation Software Toolkit enabling improved predictions of oxides of nitrogen (NOx) in high-fidelity yet computationally-tractable Computational Fluid Dynamics (CFD) analyses of combustor concepts applicable to Commercial Supersonic Transport (CST) designs. Given the technical challenges to meet the more stringent NOx emission limits at the higher CST cruising altitudes and the unique characteristics of the CST thermodynamic cycle, the proposed innovation intends to enhance the capabilities of the first-generation Software Toolkit for NASArsquo;s OpenNCC CFD code. The second-generation Software Toolkit will feature (i) enhanced predictive accuracy of the primary turbulent flame with real fuels (HyChem conventional/alternative fuels) and NOx by relaxing the dilute NOx assumption, (ii) computational efficiency, and (iii) software portability, e.g., to NASArsquo;s OpenNCC. Since CST combustor concepts will operate at higher temperatures and with higher fuel flow rates, a detailed understanding of flame dynamics is required, in particular within the context of parametric or trade studies. Given the competing performance and emission targets to be considered, a large number of design parameters needs to be considered, including both geometric parameters as well as parameters associated with combustor operation, for instance use of alternative fuels as a means to reduce NOx emissions. The significance of the innovation is that it addresses NASArsquo;s core needs for an economically feasible and environmentally acceptable propulsion technology suitable for a supersonic commercial aircraft. Historically, commercial supersonic transport has received significant opposition with respect to economic viability (e.g., due to excessive fuel consumption) and environmental impact, both in terms of sonic boom and noise generation for communities along the flight path as well as negative effects on the climate and on public health.

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.

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

National Aeronautics and Space Administration

Back to SBIR/STTR Research Awards

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