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IN EARLY 2012 THE STRUCTURE AND LIFTOFF IN COMBUSTION EXPERIMENT (SLICE) WAS CONDUCTED IN THE MICROGRAVITY SCIENCE GLOVEBOX (MSG) ABOARD THE INTERNATIONAL SPACE STATION. METHANE ETHYLENE OR A SELECTED NITROGEN DILUTION OF EACH FUEL ISSUING FROM A BURNER TUBE IN COFLOWING AIR WAS IGNITED TO FORM A LAMINAR DIFFUSION FLAME. FLOW CONDITIONS AND THE FINITE-RATE COMBUSTION CHEMISTRY CAUSED THE FLAME TO DETACH FROM THE BURNER RIM AND LIFT TO A NEW STABILIZING POSITION DOWNSTREAM. THE STRUCTURE OF THE FLAME WAS CHARACTERIZED AND THE LIFTOFF VELOCITY LIMITS WERE DETERMINED AS A FUNCTION OF THE FUEL AND BURNER DIAMETER. THE FLAME TEMPERATURE SOOT AND CH* RADICAL CONCENTRATIONS WERE MEASURED AND COMPARED WITH COMPUTATION. ALTHOUGH THE LIFTED FLAME FAR FROM THE BURNER (~10 CM) MIGHT BE STABILIZED WITH A TRIPLE-FLAME STRUCTURE I.E. A STOICHIOMETRIC DIFFUSION FLAME BASE WITH FUEL LEAN AND RICH PREMIXED BRANCHES THE STABILIZING AND LIFTING MECHANISMS OF BURNER-RIM-ATTACHED FLAMES WERE STILL LARGELY LEFT UNSTUDIED. THE GLOBAL OBJECTIVE OF THE PROPOSED RESEARCH IS TO ELUCIDATE THE DIFFUSION FLAME STABILIZING AND LIFTING MECHANISMS. THE SPECIFIC AIMS INCLUDE: (1) ANALYZE THOROUGHLY THE SLICE LIFTOFF VELOCITY LIMIT DATA TO EXTRACT GENERAL TRENDS (2) CONDUCT GROUND-BASED LIFTOFF EXPERIMENTS USING C1 C4 HYDROCARBONS TO STUDY FUEL EFFECTS (3) PERFORM COMPUTATION WITH FULL CHEMISTRY TO REVEAL THE FLAME STRUCTURE AND FLAME-FLOW INTERACTIONS LEADING TO THE LIFTOFF CONDITIONS. THE OVERALL MERIT OF THE PROPOSED RESEARCH IS FUNDAMENTAL CONTRIBUTIONS TO COMBUSTION SCIENCE AND NASA S MICROGRAVITY COMBUSTION RESEARCH THROUGH THE EFFECTIVE USE OF UNDERUTILIZED SLICE DATA ON THE LIFTOFF LIMITS AND THE RIGOROUS VALIDATION OF THE NUMERICAL METHODS INCLUDING REACTION MECHANISMS SOOT FORMATION AND RADIATION MODELS. THE PI HAS MORE THAN 20 YEARS OF EXPERIENCE AND KNOWLEDGE IN MICROGRAVITY COMBUSTION RESEARCH AND HAS SERVED AS A CO-INVESTIGATOR FOR THE SLICE PROJECT. CASE WESTERN RESERVE UNIVERSITY HAS RECENTLY EXPANDED THE FIRE AND COMBUSTION LABORATORIES EQUIPPED WITH VARIOUS FIRE TESTING INSTRUMENTS AND THE COMPUTATION WILL BE PERFORMED USING THE CASE HIGH PERFORMANCE COMPUTING CLUSTER. IF SUCCESSFUL THE PROPOSED RESEARCH WILL GIVE A SIGNIFICANT IMPACT ON THE RESEARCH AREA OF FLAME STABILIZATION WHICH HAS BEEN ONE OF MAJOR SUBJECTS OF INTEREST SINCE THE EARLY DAYS OF MODERN COMBUSTION RESEARCH STARTED SEVERAL DECADES AGO. AS A RESULT OF RECENT ADVANCES IN FLAME DIAGNOSTIC TECHNIQUES AND NUMERICAL PREDICTIVE CAPABILITIES INCLUDING COMPREHENSIVE CHEMICAL KINETICS IT IS NOW FEASIBLE TO ELUCIDATE COMPLEX FLAME-FLOW INTERACTING PHENOMENA SUCH AS FLAME STABILIZATION. A FEDERAL FINANCIAL ASSISTANCE IS NEEDED TO ACCOMPLISH SUCH AN IMPORTANT SCIENTIFIC GOAL.

$200,000FY2020National Aeronautics and Space AdministrationNASA

Case Western Reserve University, Cleveland OH

Investigators

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