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Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Quest Integrated, LLC
- Proposal award date
- Not reported
- Contract end date
- Not reported
- UEI
- S2AMPALHTDJ3
- Solicitation number
- Not reported
- Topic code
- Not reported
Research abstract
CONVENTIONAL, TURBULENT-MIXING MODELS BASED ON GRADIENT-DIFFUSION ASSUMPTIONS ARE NOT CAPABLE OF ACCURATELY PREDICTING MIXING AND REACTION RATES IN MOST PRACTICAL COMBUSTION DEVICES. FURTHERMORE, AT THE SMALL SCALES, MOST CONVENTIONAL MODELS MAKE NO DISTINCTION BETWEENTURBULENT CONVERSION AND MOLECULAR DIFFUSION. THIS DISTINCTION IS CRITICAL FOR THE ACCURATE DESCRIPTION OF THE MIXING PROCESS. IN ADDITION, IT IS KNOWN THAT TURBULENTMIXING AND ENTRAINMENT PROCESSES IN SHEAR FLOWS ARE DOMINATED BY UNSTEADY, LARGE-SCALE, VORTICAL MOTIONS. THE SPATIAL AND TEMPORAL EVOLUTION OF THESE LARGE-SCALE STRUCTURES CANNOT BE MODELED AND MUST BE EXPLICITLY COMPUTED FOR ACCURATE PREDICTIONS. PHASE I WILL EXPLORE SUBGRID MODELING TECHNIQUES FOR USE IN LARGE-EDDY SIMULATION (LES) OF REACTING FLOWS. IN PARTICULAR, A MODEL FOR MIXING AND CHEMICAL REACTIONS AT THE SUBGRID LEVEL IN BOTH LOW- AND HIGH-SPEED FLOWS WILL BE DEVELOPED BASED ON KERSTEIN'S LINEAR-EDDY APPROACH. LES OF INCOMPRESSIBLE, TWO-DIMENSIONAL MIXING LAYERS WILL BE PERFORMED, AND THE RESULTS WILL BE COMPARED WITH HIGH-RESOLUTION, DIRECT NUMERICAL SIMULATIONS AND AVAILABLE EXPERIMENTAL DATA TO ASSESS THE PROPOSED SUBGRID MODEL. THIS MODEL WOULD BE EXTENDED TO STUDY THREE-DIMENSIONAL, COMPRESSIBLE REACTING FLOWS WITH HEAT RELEASE IN PHASE II. CONVENTIONAL, TURBULENT-MIXING MODELS BASED ON GRADIENT-DIFFUSION ASSUMPTIONS ARE NOT CAPABLE OF ACCURATELY PREDICTING MIXING AND REACTION RATES IN MOST PRACTICAL COMBUSTION DEVICES. FURTHERMORE, AT THE SMALL SCALES, MOST CONVENTIONAL MODELS MAKE NO DISTINCTION BETWEENTURBULENT CONVERSION AND MOLECULAR DIFFUSION. THIS DISTINCTION IS CRITICAL FOR THE ACCURATE DESCRIPTION OF THE MIXING PROCESS. IN ADDITION, IT IS KNOWN THAT TURBULENTMIXING AND ENTRAINMENT PROCESSES IN SHEAR FLOWS ARE DOMINATED BY UNSTEADY, LARGE-SCALE, VORTICAL MOTIONS. THE SPATIAL AND TEMPORAL EVOLUTION OF THESE LARGE-SCALE STRUCTURES CANNOT BE MODELED AND MUST BE EXPLICITLY COMPUTED FOR ACCURATE PREDICTIONS. PHASE I WILL EXPLORE SUBGRID MODELING TECHNIQUES FOR USE IN LARGE-EDDY SIMULATION (LES) OF REACTING FLOWS. IN PARTICULAR, A MODEL FOR MIXING AND CHEMICAL REACTIONS AT THE SUBGRID LEVEL IN BOTH LOW- AND HIGH-SPEED FLOWS WILL BE DEVELOPED BASED ON KERSTEIN'S LINEAR-EDDY APPROACH. LES OF INCOMPRESSIBLE, TWO-DIMENSIONAL MIXING LAYERS WILL BE PERFORMED, AND THE RESULTS WILL BE COMPARED WITH HIGH-RESOLUTION, DIRECT NUMERICAL SIMULATIONS AND AVAILABLE EXPERIMENTAL DATA TO ASSESS THE PROPOSED SUBGRID MODEL. THIS MODEL WOULD BE EXTENDED TO STUDY THREE-DIMENSIONAL, COMPRESSIBLE REACTING FLOWS WITH HEAT RELEASE IN PHASE II.
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
46 SBIR/STTR records share this UEI (1989–2016). Reported award amounts total $10,954,501. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration, National Science Foundation, Department of Commerce, Department of Transportation, Department of Energy
Agency intelligence
National Aeronautics and Space Administration
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