Federal Contractor Profile
Cfd Research Corporation
$220M obligated·409 awards·7 agencies·14 NAICS
Federal Contracts
Showing contracts 401–450 of 534 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Apr 23, 2018 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865018C2216 | 541715 | IGF::OT::IGF REAL TIME AEROSERVOELASTICITY SIMULATION TOOL FOR AIRCRAFT LIFE PREDICTION - SBIR II | $187K |
| Apr 12, 2018 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $295K |
| Mar 27, 2018 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017C2036 | 541712 | IGF::OT::IGF DEVELOPMENT OF ADAPTIVE CLOSURE MODELS FOR LARGE EDDY SIMULATIONS OF LEAN BLOW-OUT CONDITIONS | $187K |
| Mar 23, 2018 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0018 | 541712 | IGF::CT::IGF ARMY SBIR PHASE II(C) AWARD | $500K |
| Mar 3, 2018 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $1.6M |
| Feb 23, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX15CD03C | 541712 | IGF::OT::IGF THE OVERALL GOAL OF THE PROJECT IS TO DEVELOP RELIABLE REDUCED ORDER MODELING TECHNOLOGIES TO AUTOMATICALLY GENERATE PARAMETER-VARYING (PV), AEROSERVOELASTIC (ASE) REDUCED-ORDER MODELS (ROMS) FOR AEROSTRUCTURAL SENSING AND CONTROL. IN PHASE 1, BOTH EQUATION-BASED AND DATA-DRIVEN PV ROM TECHNOLOGIES WERE DEVELOPED AND PROOF-OF-PRINCIPLE WAS SUCCESSFULLY DEMONSTRATED. A SET OF CAREFULLY SELECTED ROM ALGORITHMS AND MODEL COUPLING SCHEMES WERE DEVELOPED IN AN INTEGRATED ARCHITECTURE TO GENERATE PV ASE ROMS. CRITICAL EVIDENCE WAS ESTABLISHED IN NASA RELEVANT CASE STUDIES THAT ROMS ENABLE UNPRECEDENTED SPEEDUP AND ACCURACY FOR AIRCRAFT ASE ANALYSIS. PV ASE ROMS FOR X-56A MUTT MODELS IN THE CURRENT MISSION WERE DEVELOPED, WHICH DEMONSTRATED>10X REDUCTION IN THE NUMBER OF STATES AND PRECISE CAPTURE OF VEHICLE DYNAMICS AT VARIOUS FLIGHT CONDITIONS. IN PHASE 2, SOFTWARE WILL BE EXPANDED AND REFINED FOR ENHANCED PERFORMANCE AND FUNCTIONALITY. ROM ALGORITHMS WILL BE OPTIMIZED IN TERMS OF EFFICIENCY FOR MIMO SYSTEMS, CONSISTENT STATE REPRESENTATION, PV CAPABILITIES IN A BROAD FLIGHT ENVELOPE. PV STRUCTURAL ROM WILL ALSO BE DEVELOPED TO CONSIDER CHANGES IN MODAL PARAMETERS AT VARIOUS FLIGHT CONDITIONS. THE STRATEGIES FOR INTEGRATING ROMS, SENSORS AND ACTUATORS WITH CONTROL DESIGN FOR ASE STUDIES WILL BE TAILORED TO MEET VARIOUS NEEDS IN NASA. A MODULAR SOFTWARE ENVIRONMENT WILL BE DEVELOPED WITH FACILE INTERFACING TO NASA TOOLS FOR TECHNOLOGY INSERTION AND TRANSITION. ROM SOFTWARE WILL BE EXTENSIVELY VALIDATED AND DEMONSTRATED FOR ASE AND FLIGHT CONTROL ANALYSIS OF THE CURRENT X-56A MUTT MODEL, ITS FUTURE RELEASE, AND OTHER RELEVANT AIRCRAFTS. | $200K |
| Feb 21, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P0775 | 541715 | THE OBJECTIVE OF THIS EFFORT IS TO EXPAND THE EXISTING CAPABILITIES OF THE PARAMETER-VARYING AEROSERVOELASTIC ROM FOR FAST AND RAPID LOAD PREDICTION AND STRUCTURAL ANALYSIS THAT HAVE BEEN DEVELOPED UNDER THE ONGOING PHASE II PROJECT. THIS PHASE III EFFORT WILL FOCUS ON 1. DEVELOPMENT OF ROM-BASED LOAD ANALYSIS CAPABILITIES WITH THE GOAL OF IMPROVING THE EFFICIENCY AND THE FIDELITY OF THE VARIOUS STEPS INVOLVED IN THE LOAD ANALYSIS CYCLE. 2. EXTENSIVE DEMONSTRATION OF THE ROM CAPABILITIES USING PRACTICAL PROBLEMS IN STRUCTURAL AND AERODYNAMIC LOAD ANALYSIS BEING UNDERTAKEN BY NASA/MSFC TO SUPPORT THE SLS PROGRAM. 3. INTEGRATION OF STRUCTURAL DYNAMICS DATA REDUCTION AND DATA-DRIVEN ROMS WITHIN A SINGLE SOFTWARE ENVIRONMENT AND INSERT THE TECHNOLOGY IN THE EXISTING NASA/MSFC WORKFLOW. | $100K |
| Feb 20, 2018 | Department of DefenseW6QK ACC-RSA | W31P4Q17C0025 | 541712 | IGF::OT::IGF ARMY SBIR PHASE II FOR WORK ENTITLED - A HYPERSONIC ENVIRONMENT ANALYSIS TOOL (HEAT). | $483K |
| Feb 16, 2018 | Department of DefenseW6QK ACC-RSA | W31P4Q17C0030 | 541712 | IGF::OT::IGF ARMY SBIR PHASE II FOR THE EFFORT ENTITLED "REAL-TIME VOLUMETRIC WEATHER/PROPAGATION LOSS MODEL" | $511K |
| Jan 24, 2018 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014717C7604 | 541712 | IGF::OT::IGF SBIR/STTR PHASE I RESEARCH&DEVELOPMENT | $25K |
| Jan 24, 2018 | Department of DefenseW6QK ACC-APG NATICK | W911QY17C0008 | 541712 | IGF::OT::IGF PHASE II SBIR | $500K |
| Jan 17, 2018 | Department of DefenseW6QK ACC-APG NATICK | W911QY16P0389 | 541712 | FINAL TECHNICAL REPORT BASE PERIOD IGF::OT::IGF | $50K |
| Jan 3, 2018 | Department of DefenseFA9101 AEDC PKP PROCRMNT BR | FA910118C0021 | 541715 | IGF::OT::IGF CFDRC AF161-024 PHASE II PREDICTION OF HYPERSONIC BOUNDRY-LAYER TRANSITION IN WIND TUNNELS AND FLIGHT | $563K |
| Dec 22, 2017 | Department of DefenseW6QK ACC-APG DURHAM | W911NF17C0026 | 541712 | IGF::OT::IGF | $500K |
| Dec 19, 2017 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001418C7004 | 541715 | IGF::CT::IGF | $500K |
| Dec 6, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH18C0047 | 541715 | IGF::OT::IGF ARMY STTR PHASE I TOPIC A17A-T022 PROPOSAL A17A-022-0069 BIOFIDELIC RAT TESTING DEVICE (RTD) TO MEASURE BLAST EXPOSURE AND LOADINGS FOR TBI | $150K |
| Dec 5, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865018C2216 | 541715 | IGF::OT::IGF REAL TIME AEROSERVOELASTICITY SIMULATION TOOL FOR AIRCRAFT LIFE PREDICTION - SBIR II | $563K |
| Oct 25, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865018C6870 | 541715 | GLOBAL LOCAL MODEL OF AIRCRAFT OCCUPANT SAFETY ASSESSMENT DURING EJECTION - SBIR II | $750K |
| Oct 11, 2017 | Department of DefenseFA9101 AEDC PKP PROCRMNT BR | FA910118C0050 | 541715 | IGF::OT::IGF STTP 2016-02 COMPUTATIONAL MODEL FOR ELECTRODE EROSION BY HIGH-PRESSURE MOVING ARCS | $800K |
| Sep 28, 2017 | Department of DefenseFA9300 AFTC PZR | FA930017C2501 | 541712 | IGF::OT::IGF STTR PHASE II MEASUREMENT AND MODELING OF SURFACE COKING IN FUEL-FILM COOL | $187K |
| Sep 27, 2017 | Department of DefenseW6QK ACC-APG | W911SR17C0060 | 541511 | IGF::OT::IGF SMARTPHONE APP FOR MASK SIZING YEAR 1 | $547K |
| Sep 25, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0177 | 541712 | IGF::OT::IGF DHA SBIR 2ND PHASE II PROPOSAL H2-0256 TOPIC DHP16-005 PORTABLE IRON SCREENING SYSTEM FOR POINT-OF-CARE IRON STATUS DETERMINATION ERMS 17124018 | $1000K |
| Sep 22, 2017 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $505K |
| Sep 22, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0216 | 541712 | IGF::OT::IGF DHA SBIR 2ND PHASE - H2-0266 | $1000K |
| Sep 19, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC17C0039 | 541712 | IGF::OT::IGFCHEMICAL CONTAMINATION OF SPACECRAFT COMPONENTS AS WELL AS THERMAL AND FORCE LOADING FROM FIRING LIQUID PROPELLANT THRUSTERS ARE CRITICAL CONCERNS FOR IN-SPACE PROPULSION APPLICATIONS. GAS MOLECULAR CONTAMINATION AND LIQUID DROPLET DEPOSITION DUE TO INCOMPLETE COMBUSTION THREATEN TO DAMAGE SURFACE MATERIALS, SENSITIVE INSTRUMENTS AND OPTICAL SENSORS, AND POSES MAJOR RISKS FOR MISSION SUCCESS. LIQUID PROPELLANT THRUSTERS OPERATE IN SPACE AT NEAR-VACUUM CONDITIONS, AND CONTAMINANTS TRAVERSE A COMPLEX MIXED CONTINUUM-RAREFIED ENVIRONMENT UPON EXITING THE THRUSTER NOZZLE. CURRENT CFD MODELING CAPABILITIES FOR IN-SPACE PROPULSION ANALYSIS HAVE MADE GREAT STRIDES, BUT FALL SHORT OF PROVIDING THE FIDELITY REQUIRED TO SIMULATE THE CONTAMINANT TRANSPORT AROUND THE SPACECRAFT WITH SUFFICIENT EFFICIENCY AND ACCURACY. THIS STTR WILL DEVELOP AND DELIVER AN INNOVATIVE COMPUTATIONAL ARCHITECTURE FOR PREDICTION OF PLUME FLOW IMPINGEMENT AND CONTAMINANT DISPERSAL THROUGH MIXED FLOW ENVIRONMENTS FOR IN-SPACE PROPULSION ANALYSIS. CFDRC WILL SUPPLEMENT THE MASSIVELY PARALLEL LOCI FRAMEWORK WITH A UNIFIED SOLVER FOR PREDICTION OF MIXED CONTINUUM-RAREFIED FLOWS WITH CONTAMINANT DISPERSAL. THIS WILL ENABLE BETTER UNDERSTANDING OF THERMAL AND FORCE LOADING AND CONTAMINATION OF SPACECRAFT COMPONENTS, AND ENABLE DESIGN OF SAFER NEXT-GENERATION IN-SPACE PROPULSION SYSTEMS. A PROOF-OF-CONCEPT WAS DEVELOPED AND SUCCESSFULLY DEMONSTRATED DURING PHASE I FOR IN-SPACE THRUSTER PLUME CONTAMINATION ENVIRONMENTS. PHASE II WILL DELIVER PRODUCTION CONTINUUM-KINETIC-PARTICLE PREDICTIVE CAPABILITIES WITH ADAPTIVE MESH/ALGORITHM REFINEMENT FOR MULTI-COMPONENT MOLECULAR GASES, WHICH WILL PROVIDE NASA WITH NEXT-GENERATION TOOLS FOR DETAILED INVESTIGATIONS OF CONTAMINANT ENVIRONMENTS FOR SPACECRAFT CONFIGURATIONS. | $750K |
| Sep 18, 2017 | Department of DefenseW6QK ACC-RSA | W31P4Q17C0128 | 541712 | CFD RESEARCH CORPORATION FOR PERFORMANCE OF THE PWS ENTITLED, 2016 RAPID INNOVATION FUND (RIF) ARMY20-PEOMS01-3273 "PASSIVELY THROTTLED SOLID ROCKET MOTOR", | $2.9M |
| Sep 18, 2017 | Department of DefenseW6QK ACC-RSA | W31P4Q17C0147 | 541712 | IGF::OT::IGF ARMY SBIR PHASE II FOR THE EFFORT ENTITLED "SOFTWARE TOOL FOR ACCURATE AND RAPID LOAD ANALYSIS AND DESIGN OF EXPERIMENTS". | $499K |
| Sep 18, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0202 | 541712 | IGF::OT::IGF. ARMY PHASE I PROPOSAL A171-068-0609 TITLED "VASCULARIZATION OF THICK TISSUE CONSTRUCTS FOR REGENERATIVE MEDICINE APPLICATIONS." | $100K |
| Sep 14, 2017 | Department of DefenseFA9550 AFRL AFOSR | FA955017P0018 | 541712 | IGF::OT::IGF SBIR COMPUTATIONALLY EFFICIENT, ACCURATE&UNCERTAINTY CHARACTERIZED CHEMICAL KINETICS FOR HYDROCARBON | $150K |
| Sep 13, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0108 | 541712 | IGF::CT::IGF SBIR PHASE I AWARD DYNAMIC WARFIGHTER AVATARS WITH COMPLETE ARTICULATED ANATOMY | $150K |
| Sep 7, 2017 | Department of Health and Human ServicesNATIONAL INSTITUTES OF HEALTH NIDA | HHSN271201700044C | 541712 | IGF::OT::IGF SMARTPLATE TECHNOLOGY FOR ADVANCED CELLULAR (STAC-M) | $1.5M |
| Aug 29, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017C2036 | 541712 | IGF::OT::IGF DEVELOPMENT OF ADAPTIVE CLOSURE MODELS FOR LARGE EDDY SIMULATIONS OF LEAN BLOW-OUT CONDITIONS | $563K |
| Aug 23, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX14CK11C | 541712 | IGF::OT::IGF THE LIBERATION OF PARTICLES INDUCED BY ROCKET PLUME FLOW FROM SPACECRAFT LANDING ON UNPREPARED REGOLITH OF THE MOON, MARS, AND OTHER DESTINATIONS POSES HIGH MISSION RISKS FOR ROBOTIC AND HUMAN EXPLORATION ACTIVITIES. THIS PROCESS OCCURS IN A COMBINATION OF "EXTREME ENVIRONMENTS" THAT COMBINE LOW GRAVITY, LITTLE OR NO ATMOSPHERE, ROCKET EXHAUST GAS FLOW THAT IS SUPERSONIC AND PARTIALLY RAREFIED, AND UNUSUAL GEOLOGICAL AND MECHANICAL PROPERTIES OF HIGHLY IRREGULAR SURFACE REGOLITH. CFDRC AND THE UNIVERSITY OF FLORIDA WILL DELIVER UNIQUE PLUME DRIVEN EROSION SIMULATION SOFTWARE FOR SUCH ENVIRONMENTS BY COMBINING NOVEL GRANULAR PHYSICS SIMULATION MODULES DEVELOPED BY UF WITH MULTI-PHASE GAS-GRANULAR FLOW SIMULATION SOFTWARE DEVELOPED BY CFDRC. GRANULAR FLOW CONSTITUTIVE MODELS, FORMULATED THROUGH FIRST-PRINCIPLE 3-D DISCRETE ELEMENT METHOD PARTICLE KINETICS AND IMPLEMENTED IN AN EFFICIENT EULERIAN GAS-GRANULAR FLOW SOLVER ARE THE FOUNDATION OF THIS SOFTWARE. THE FIDELITY OF THESE SIMULATIONS WILL BE ADVANCED TOWARDS SIMULATING PARTICLE COMPOSITIONS WITH BROAD SHAPE AND SIZE VARIATIONS. NOVEL PARTICLE KINETICS MODELING CONCEPTS WILL BE APPLIED TO FORMULATE GRANULAR FLOW PHYSICS MODELS FOR BOTH, REALISTIC IRREGULAR PARTICLE SHAPES AND DISPERSED PARTICLE SIZE DISTRIBUTIONS. PHASE I DEMONSTRATED THE SUCCESSFUL IMPLEMENTATION AND VALIDATION OF IRREGULAR GRANULAR SHAPE PHYSICS MODELING IN CFDRC'S GASGRANULAR MULTI-PHASE FLOW SOLVER. AN APPROACH FOR EXTENSION TO POLY-DISPERSE PARTICLE MIXTURE SIMULATIONS WAS ALSO DEVELOPED. FULL INTEGRATION OF THESE MODELS IN PHASE II WILL ENABLE THE SIMULATION OF GAS FLOW INTERACTION WITH POLY-DISPERSE, IRREGULAR SHAPED PARTICLE MATERIALS. EXTENSIVE VERIFICATION, VALIDATION, AND APPLICATION DEMONSTRATIONS WILL BE PERFORMED. THE PROPOSED TECHNOLOGY DEVELOPMENT WILL RESULT IN UNPRECEDENTED COMPUTER MODELING CAPABILITY FOR PREDICTING LIBERATION AND FLOW OF REALISTIC GRANULAR MATERIAL COMPOSITIONS IN EXTREME EXTRA-TERRESTRIAL ENVIRONMENTS. | $246K |
| Aug 15, 2017 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $410K |
| Aug 14, 2017 | Department of DefenseFA9101 AEDC PKP PROCRMNT BR | FA910116C0001 | 541712 | IGF::OT::IGF CFD RESEARCH CORP SBIR 2 | $250K |
| Aug 10, 2017 | Department of DefenseFA9101 AEDC PKP PROCRMNT BR | FA910117P0091 | 541712 | IGF::OT::IGF CFD SBIR 1 | $150K |
| Aug 4, 2017 | Department of DefenseW6QK ACC-RSA | W31P4Q17C0129 | 541712 | IGF::OT::IGF ARMY SMALL BUSINESS INNOVATION RESEARCH PHASE I EFFORT ENTITLED, "AIR MISSILE DEFENSE WEATHER MANAGEMENT" | $100K |
| Jul 26, 2017 | Department of DefenseW6QK ACC-APG DURHAM | W911NF17P0075 | 541712 | IGF::OT::IGF PHASE I FIRST MONTHLY TECHNICAL REPORT-- | $100K |
| Jul 25, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0095 | 541712 | IGF::OT::IGF DHP PHASE II PROPOSAL H2-0207 TOPIC DHP16-001 PERSONALIZED WARRIOR HEALTH AVATAR ERMS 16117001 | $999K |
| Jul 20, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC17P0318 | 541511 | IGF::OT::IGFANNUAL RENEWAL OF SOFTWARE CFD-ACE | $116K |
| Jul 18, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016C5004 | 541712 | IGF::OT::IGF SBIR II: INTEGRATED SOFTWARE TO PREDICT MATERIAL DEGRADATION IN SPECIAL TECHNOLOGY COATINGS | $187K |
| Jul 12, 2017 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833517C0088 | 541712 | SBIR PII.5 R&D. IGF::OT::IGF | $456K |
| Jul 11, 2017 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $575K |
| Jul 11, 2017 | Department of DefenseFA8651 AFRL RWK | FA865117P0128 | 541712 | IGF::OT::IGF STTR I EXTENDING MOLECULAR SIMULATION TO GRAIN SCALE FOR SIMULATING RESPONSE OF ENERGETIC MATERIAL UNDER H | $150K |
| Jul 6, 2017 | Department of DefenseDEFENSE THREAT REDUCTION AGENCY | HDTRA117P0040 | 541712 | IGF::OT::IGF - STTR PHASE I NOVEL MIXED-MADE TCAD-COMMERCIAL PDK INTEGRATED FLOW FOR RADIATION HARDENING BY DESIGN. | $150K |
| Jun 29, 2017 | Department of DefenseFA9550 AFRL AFOSR | FA955017C0017 | 541712 | IGF::OT::IGF"(SBIR II) A DESIGN AUTOMATION TOOL FOR INTEGRATED NANOPHOTONICS BASED ON COMPACT MODELING AND MODEL ORDER RE | $750K |
| Jun 20, 2017 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $999K |
| Jun 8, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CC34P | 541712 | IGF::OT::IGF ENVIRONMENTAL BARRIER COATINGS (EBC) PREVENT OXIDATION OF CERAMIC MATERIALS IN REACTIVE, HIGH TEMPERATURE ENVIRONMENTS SUCH AS THE EXHAUST REGIONS OF GAS TURBINE ENGINES. CFDRC PROPOSES TO A DEVELOP A PHYSICS BASED MODEL OF AN EBC SYSTEM INTERACTING WITH THE FLOW ENVIRONMENT TO PROVIDE A MEANS TO GAIN BETTER UNDERSTANDING OF THE DYNAMIC PROCESSES THAT EFFECT EBC DURABILITY AND PERFORMANCE UNDER PROPULSION CONDITIONS. THE MODEL WILL USE COMPUTATIONAL FLUIDS DYNAMICS TO ESTABLISH THE CONDITIONS AND SPECIES CONCENTRATIONS ACROSS THE SURFACE OF THE STRUCTURE. STRUCTURAL MODELS OF THE PART BASED ON THE FINITE ELEMENT METHOD (FEM) WILL BE USED TO ESTABLISH THE THERMAL AND MECHANICAL LOADS ACTING ON THE COATING MATERIAL. THE RESPONSE OF THE COATING MATERIALS WILL BE MODELED AT THE MICROSCALE WHERE EACH COMPONENT OF THE COATING SYSTEM IS DISCRETELY RESOLVED. THE MICROMECHANICS MODEL IS BASED ON PERIDYNAMICS, A MESH FREE THEORY OF CONTINUUM MECHANICS THAT IS WELL SUITED TO MODEL DAMAGE IN BRITTLE CERAMIC MATERIALS. RECENT DEVELOPMENTS IN PERIDYNAMICS ADAPTED THE METHOD TO MODEL DIFFUSIVE TRANSPORT COUPLED WITH DEFORMATION AND DAMAGE, WHICH WILL BE APPLIED TO PREDICT THE DISTRIBUTION OF REACTIVE SPECIES OVER TIME THROUGH THE COATING SYSTEM. | $125K |
| Jun 5, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CL49P | 541712 | IGF::OT::IGF DESPITE THE RAPID COMMERCIALIZATION OF ADDITIVE MANUFACTURING TECHNOLOGY SUCH AS SELECTIVE LASER MELTING, SLM, THERE ARE GAPS IN MODELS FOR MATERIAL MICROSTRUCTURE AND PROPERTY PREDICTION THAT SLOW QUALIFICATION AND CERTIFICATION. IMPROVEMENTS IN COUPLING MICROSTRUCTURE PREDICTION MODELS TO LOCAL PROCESS CONDITIONS, VALIDATION, AND CONTROL OF MATERIAL MICROSTRUCTURE ARE REQUIRED TO MATURE THE STATE OF THE ART. TO ADDRESS THESE NEEDS, CFDRC IN PARTNERSHIP WITH ARIZONA STATE UNIVERSITY WILL DEVELOP AND APPLY MODELING AND SIMULATION TOOLS FOR PREDICTION AND CONTROL OF MICROSTRUCTURE IN SLM FABRICATED PARTS. THE PHASE I EFFORT WILL ESTABLISH CRITICAL SOFTWARE ELEMENTS, MODELING METHODOLOGY, AND EXPERIMENTAL DATA ANALYSIS REQUIRED FOR PHASE II. WE WILL DEMONSTRATE THE FEASIBILITY OF HIGH-FIDELITY MODELS THAT ARE CAPABLE OF PREDICTING THE FORMATION OF KEY METALLURGICAL MICROSTRUCTURES OBSERVED IN SLM ADDITIVE MANUFACTURING PROCESSES AS A FUNCTION OF THE LOCAL THERMAL ENVIRONMENT AT DIFFERENT LOCATIONS WITHIN THE AS-BUILT COMPONENT, REDUCED MODELS FOR MAPPING PROCESS CONDITIONS TO ADDITIONAL MICROSTRUCTURE FEATURES IMPACTING MATERIAL QUALITY, AND POTENTIALLY CONTROLLING MATERIAL QUALITY THROUGHOUT A SAMPLE AS-BUILT PART. THE PHASE II PROGRAM WILL FOCUS ON THE DEVELOPMENT OF EFFICIENT, VALIDATED HIGH-FIDELITY SIMULATION CODES AND REDUCED MODELS PROVIDING THE MEANS TO REDUCE VARIABILITY IN AS-BUILT MATERIAL MICROSTRUCTURE AND PROPERTIES, AND CULMINATE WITH THE DELIVERY TO THESE TOOLS TO NASA RESEARCHERS AND OTHER STAKEHOLDERS. | $125K |
| Jun 5, 2017 | Department of DefenseW6QK ACC-RSA | W31P4Q17C0039 | 541712 | IGF::OT::IGF--ARMY SBIR PHASE II, ENTITLED, "AUTOMATED AND DYNAMIC ACCESS CONTROL (ADAC) TO CRITICAL MISSILE SYSTEMS DATA", CFD RESEARCH CORP. | $362K |
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