SBIR/STTR Research Award

A NEW UNSTEADY MIXING MODEL TO PREDICT NOX PRODUCTION DURINGRAPID MIXING IN A DUAL-STAGE COMBUSTOR

Award identifier 838944d554473c2bce1d3ffd84273451982e4ef4b13b6c3cb7064adf236d70cdAwarding agency National Aeronautics and Space Administration

Award amount

$464,850

Program and phase

SBIR · Phase II

Award year

1992

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Waterjet Technology Inc
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

AN ADVANCED GAS TURBINE ENGINE TO POWER SUPERSONIC TRANSPORTAIRCRAFT IS CURRENTLY UNDER STUDY. IN ADDITION TO HIGH COMBUSTION-EFFICIENCY REQUIREMENTS, ENVIRONMENTAL CONCERNS HAVE PLACED STRINGENT RESTRICTIONS ON THE POLLUTANT EMISSIONS FROM THESE ENGINES. A COMBUSTOR DESIGN WITH THE POTENTIAL FOR MINIMIZING POLLUTANTS SUCH AS NOX EMMISSIONS IS UNDERGOING EXPERIMENTAL EVALUATION. A MAJOR TECHNICAL ISSUE IN THE DESIGN OF THIS COMBUSTOR IS HOW TO RAPIDLY MIX THE HOT, FUEL-RICH PRIMARY-ZONE PRODUCT WITH THE SECONDARY DILUENT AIR TO OBTAIN A FUEL-LEAN MIXTURE FOR COMBUSTION IN THE SECONDARY STAGE. NUMERICAL PREDICTIONS USING STEADY-STATE METHODS CANNOT ACCOUNT FOR THE UNSTEADY PHENOMENA IN THE MIXING REGION. THEREFORE, THIS PROJECT ADDRESSES A NOVEL UNSTEADY MIXING MODEL THAT CAN BE USED TO EVALUATE MIXING AND COMBUSTION, INCLUDING NO PRODUCTION WITHIN THE MIXING REGION. THIS MODEL WILL BE DEVELOPED FOR USE IN CONJUNCTION WITH STEADY-STATE PREDICTION METHODS AND THUS WILL HAVE THE POTENTIAL FOR PROVIDING AN IMPROVED ENGINEERING DESIGN ANALYSIS TOOL. THE CAPABILITY OF THIS MODEL WILL BE DEMONSTRATED IN PHASE I WITH THE EVENTUAL OBJECTIVE OF COUPLING THE MODEL TO A STEADY-STATE SOLVER IN PHASE II. AN ADVANCED GAS TURBINE ENGINE TO POWER SUPERSONIC TRANSPORTAIRCRAFT IS CURRENTLY UNDER STUDY. IN ADDITION TO HIGH COMBUSTION-EFFICIENCY REQUIREMENTS, ENVIRONMENTAL CONCERNS HAVE PLACED STRINGENT RESTRICTIONS ON THE POLLUTANT EMISSIONS FROM THESE ENGINES. A COMBUSTOR DESIGN WITH THE POTENTIAL FOR MINIMIZING POLLUTANTS SUCH AS NOX EMMISSIONS IS UNDERGOING EXPERIMENTAL EVALUATION. A MAJOR TECHNICAL ISSUE IN THE DESIGN OF THIS COMBUSTOR IS HOW TO RAPIDLY MIX THE HOT, FUEL-RICH PRIMARY-ZONE PRODUCT WITH THE SECONDARY DILUENT AIR TO OBTAIN A FUEL-LEAN MIXTURE FOR COMBUSTION IN THE SECONDARY STAGE. NUMERICAL PREDICTIONS USING STEADY-STATE METHODS CANNOT ACCOUNT FOR THE UNSTEADY PHENOMENA IN THE MIXING REGION. THEREFORE, THIS PROJECT ADDRESSES A NOVEL UNSTEADY MIXING MODEL THAT CAN BE USED TO EVALUATE MIXING AND COMBUSTION, INCLUDING NO PRODUCTION WITHIN THE MIXING REGION. THIS MODEL WILL BE DEVELOPED FOR USE IN CONJUNCTION WITH STEADY-STATE PREDICTION METHODS AND THUS WILL HAVE THE POTENTIAL FOR PROVIDING AN IMPROVED ENGINEERING DESIGN ANALYSIS TOOL. THE CAPABILITY OF THIS MODEL WILL BE DEMONSTRATED IN PHASE I WITH THE EVENTUAL OBJECTIVE OF COUPLING THE MODEL TO A STEADY-STATE SOLVER IN PHASE II.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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