Federal Contractor Profile
Cfd Research Corporation
$220M obligated·409 awards·7 agencies·14 NAICS
Federal Contracts
Showing contracts 351–400 of 534 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Mar 28, 2019 | Department of DefenseDEFENSE THREAT REDUCTION AGENCY | HDTRA119C0031 | 541715 | PASSIVE, MICROSCALE, DISTRIBUTABLE SENSORS FOR IONIZING RADIATION DETECTION SMALL BUSINESS TECHNOLOGY PHASE II | $746K |
| Mar 26, 2019 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014719C7075 | 541715 | STTR PHASE I RESEARCH&DEVELOPMENT - NON-INTRUSIVE UNCERTAINTY IDENTIFICATION AND QUANTIFICATION FRAMEWORK FOR HYPERSONIC FLIGHTS | $100K |
| Mar 26, 2019 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833519C0177 | 541715 | RESEARCH AND DEVELOPMENT IGF::OT::IGF | $375K |
| Feb 12, 2019 | 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 | $187K |
| Feb 6, 2019 | 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 | $250K |
| Feb 1, 2019 | Department of the InteriorIBC ACQ SVCS DIRECTORATE (00004) | 140D0419C0040 | 541715 | IGF::OT::IGF MEDICAL DEVICES, TRAUMA, PROLONGED FIELD CARE, TACTICAL COMBAT CASUALTY CARE, SMART MATERIALS, REMOTE MONITORING | $75K |
| Dec 20, 2018 | National Aeronautics and Space AdministrationNASA AMES RESEARCH CENTER | 80ARC019F0004 | 541715 | IGF::OT::IGF THE PURPOSE OF THIS TASK ORDER IS FOR THE CONTRACTOR TO PROVIDE AN INFORMATION TECHNOLOGY (IT) SECURITY MANAGEMENT PLAN IN ACCORDANCE WITH NFS CLAUSE 1852.204-76. | $5K |
| Dec 17, 2018 | Department of DefenseW6QK ACC-APG | W911SR17C0060 | 541511 | IGF::OT::IGF SMARTPHONE APP FOR MASK SIZING YEAR 1 | $503K |
| Dec 12, 2018 | Department of DefenseFA9101 AEDC PKP PROCRMNT BR | FA910119P0026 | 541715 | AEROELASTIC VULNERABILITY ASSESSMENT | $150K |
| Dec 11, 2018 | Department of DefenseW6QK ACC-APG DURHAM | W911NF19P0002 | 541715 | IGF::OT::IGF STTR PHASE I | $150K |
| Nov 27, 2018 | 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." | $50K |
| Nov 20, 2018 | Department of DefenseW6QK ACC-RSA | W9113M19C0061 | 541715 | IGF::OT::IGF SBIR PHASE II BASE LABOR "NOVEL CATHODES FOR HIGH CAPACITY THERMAL BATTERY". | $516K |
| Nov 15, 2018 | Department of DefenseFA9101 AEDC PKP PROCRMNT BR | FA910119C0004 | 541715 | SBIR COMMERCIALIZATION READINESS PROGRAM-COMBUSTION AIR HEAT | $4.1M |
| Oct 23, 2018 | Department of DefenseFA8651 AFRL RWK | FA865119P0015 | 541715 | A SIMULATION FRAMEWORK OF MULTI-OBJECTIVE EVOLUTIONARY ALGORITHMS AND SURROGATE-BASED OPTIMIZATION FOR GUIDED WEAPONS | $150K |
| Oct 22, 2018 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV19C0003 | 541715 | IGF::OT::IGF PHASE 1 SBIR RESEARCH FOR TO DEVELOP AN INNOVATIVE COMPUTATIONAL FLUID DYNAMICS (CFD) AND MODEL ORDER REDUCTION (MOR) | $100K |
| Oct 16, 2018 | Department of DefenseNAVAL AIR WARFARE CENTER | N6893619C0017 | 541715 | IGF::OT::IGF; SBIR PHASE 1 AWARD TO CDF RESEARCH CORP. | $125K |
| Sep 29, 2018 | Department of DefenseFA2487 AFTC PZZD (EGLIN) | FA248716C0327 | 541380 | IGF::OT::IGF SMALL BUSINESS INNOVATION RESEARCH (SBIR II) - PHYSICS BASED FAST RUNNING TOOL | $25K |
| Sep 27, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0208 | 541715 | LAUNCH VEHICLES EXPERIENCE EXTREME ACOUSTIC LOADS DOMINATED BY ROCKET PLUME INTERACTIONS WITH GROUND STRUCTURES DURING LIFTOFF, WHICH CAN PRODUCE DAMAGING VIBRO-ACOUSTIC LOADS ON THE VEHICLE AND PAYLOADS IF NOT PROPERLY UNDERSTOOD AND MITIGATED AGAINST. EXISTING CAPABILITIES FOR MODELING TURBULENT PLUME PHYSICS ARE TOO DISSIPATIVE TO ACCURATELY RESOLVE THE ACOUSTIC PROPAGATION AND DETAILED VEHICLE AFT-END ACOUSTICS RELEVANT TO HYDROGEN POP DEFLAGRATION AND GEOMETRIC ATTENUATION. HIGHER FIDELITY ANALYSIS TOOLS ARE CRITICALLY NEEDED TO DESIGN MITIGATION MEASURES (E.G. WATER DELUGE) AND GROUND STRUCTURES FOR CURRENT AND FUTURE LAUNCH VEHICLES, AND TO ACCURATELY PREDICT GEOMETRIC ATTENUATION WHICH MAY ALLOW SIGNIFICANT REDUCTIONS IN SRB NOZZLE THROAT PLUG MATERIAL DENSITY REQUIREMENTS. THIS PROJECT WILL SIGNIFICANTLY ADVANCE EXISTING CAPABILITIES TO DEVELOP BREAKTHROUGH TECHNOLOGIES TO DRASTICALLY IMPROVE TRANSIENT ACOUSTIC LOADING PREDICTIONS FOR LAUNCH VEHICLES IN MOTION DURING LIFTOFF. INNOVATIVE CFD/CAA TECHNIQUES WILL BE DEVELOPED WITH RANS/LES MODELING FOR ACOUSTIC GENERATION AND DISCONTINUOUS GALERKIN MODELING FOR ACOUSTIC PROPAGATION AND VEHICLE MOTION USING IDEALLY-SUITED HIGH-ORDER SCHEMES. THIS TECHNOLOGY ENABLES: GREATLY REDUCED DISSIPATION/DISPERSION; IMPROVED MODELING OF ACOUSTIC INTERACTIONS WITH COMPLEX GEOMETRY; AND AUTOMATIC IDENTIFICATION OF TRANSIENT ACOUSTIC ENVIRONMENT INCLUDING VEHICLE MOTION. A PROOF-OF-CONCEPT WAS SUCCESSFULLY DEMONSTRATED DURING PHASE I FOR BENCHMARK APPLICATIONS AND SLS PROTOTYPE LAUNCH ENVIRONMENTS. PHASE II WILL DELIVER PRODUCTION TRANSIENT CFD/CAA CAPABILITIES FOR LAUNCH VEHICLES IN MOTION DURING LIFTOFF WITH 4TH-ORDER ACCURACY FOR NEAR-LOSSLESS ACOUSTIC MODELING OF NEAR-FIELD GEOMETRIC ATTENUATION AND LONG-DISTANCE PROPAGATION, WHICH WILL PROVIDE NASA WITH DRAMATIC INCREASES IN THE RANGE OF RESOLVABLE FREQUENCIES OVER CURRENT METHODS. | $750K |
| Sep 27, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0209 | 541715 | SOLID ROCKET MOTOR (SRM) DESIGN REQUIRES DETAILED UNDERSTANDING OF THE SLAG ACCUMULATION PROCESS IN ORDER TO: PREDICT THRUST CONTINUITY, OPTIMIZE PROPELLANT CONVERSION EFFICIENCY, PREDICT CONING EFFECTS FROM SLOSHING, AND TO ASSESS POTENTIAL ORBITAL DEBRIS (SLAG) HAZARD. CURRENT STATE-OF-THE-ART MODELS FOR SRM ENVIRONMENT DO NOT HAVE THE CAPABILITY TO SIMULATE THE ACCUMULATION AND DYNAMICS OF SLAG IN SRMS AS THEY RELY ON A LAGRANGIAN PARTICLE APPROACH THAT ARE ONLY CAPABLE OF PREDICTING THE LOCATION OF ACCUMULATION. IN PHASE I, A MULTIPHASE FRAMEWORK COMPRISING OF GAS-PHASE, A DENSE SLAG-PHASE, AND LAGRANGIAN PARTICLES REPRESENTING ALUMINUM AND ALUMINA WAS DEVELOPED AND DEMONSTRATED. PHASE II EFFORT WILL FOCUS ON EXTENDING THE DEVELOPED APPROACH BY A) INCORPORATING IMPROVED TRANSPORT AND THERMAL PROPERTIES OF SLAG, B) IMPROVING NUMERICAL APPROACH FOR SOLVING TRANSPORT OF GAS AND SLAG-PHASE IN SRM ENVIRONMENT, C) ENHANCING THE COUPLED FLOW SIMULATION CAPABILITIES INCLUDING ACCELERATED FRAME OF REFERENCE TO PREDICT SLAG DYNAMICS AND D) PROVIDING DETAILED VERIFICATION AND VALIDATION OF SUB-MODELS AND OVERALL SIMULATION CAPABILITIES. THE TOOLS DEVELOPED WILL BE OF GREAT USE IN DESIGNING AND DEVELOPING NEXT GENERATION SRMS AND EFFECT OF SLAG ON THRUST OSCILLATIONS, CONING AND DEBRIS PREDICTION. | $750K |
| Sep 25, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P3037 | 541715 | NASA/MSFC HAS A NEED FOR FURTHER ENHANCEMENTS TO THE LOCI-THRUST COMPUTATIONAL ACOUSTICS CODE (CAA) AND THE LOCI-CHEM AND LOCI-STREAM COMPUTATIONAL FLUID DYNAMICS (CFD) CODES. THE CODES WERE RECENTLY REFINED WITHIN A CFDRC STTR PHASE I, TRANSIENT ACOUSTIC ENVIRONMENT PREDICTION TOOL FOR LAUNCH VEHICLES IN MOTION DURING EARLY LIFT-OFF CONTRACT NNX17CM22P. THE LOCI-THRUST CODE WAS AND CONTINUES TO BE USED TO SUPPORT THE REFINEMENT OF THE SLS LIFTOFF ENVIRONMENTS. THE SIMULATIONS REQUIRED FOR THE SLS LIFT-OFF ACOUSTICS IS DIFFERENT FROM THE APPROACH ORIGINALLY PLANNED WHEN THE PHASE I SOW WAS DEVELOPED. UNIQUE ROUTINES ARE REQUIRED TO ENABLE MSFC TO PROPERLY MODEL THE SLS LIFT-OFF ACOUSTIC LOADS ON THE SLS HARDWARE. ADDITIONAL REFINEMENTS ARE NEEDED IN LOCI-CHEM AND LOCI-STREAM TO SUPPORT OTHER SIMULATIONS. | $70K |
| Sep 19, 2018 | Department of DefenseW6QK ACC-APG NATICK | W911QY18P0318 | 541714 | STTR PHASE I | $150K |
| Sep 18, 2018 | Department of Health and Human ServicesFDA OFFICE OF ACQ GRANT SVCS | 75F40118C10182 | 541715 | IGF::OT::IGF - A MULTISCALE COMPUTATIONAL FRAMEWORK FOR BIOEQUIVALENCE OF ORALLY INHALED DRUGS | $151K |
| Sep 12, 2018 | Department of Health and Human ServicesFDA OFFICE OF ACQ GRANT SVCS | 75F40118D10151 | 541715 | AN INTEGRATED MULTISCALE-MULTIPHYSICS MODELING FRAMEWORK FOR EVALUATION OF GENERIC OPHTHALMIC DRUG PRODUCTS | $160K |
| Sep 10, 2018 | Department of DefenseFA2487 AFTC PZZD (EGLIN) | FA248716C0327 | 541380 | IGF::OT::IGF SMALL BUSINESS INNOVATION RESEARCH (SBIR II) - PHYSICS BASED FAST RUNNING TOOL | $420K |
| Sep 10, 2018 | Department of DefenseFA2487 AFTC PZZD (EGLIN) | FA248716C0327 | 541380 | IGF::OT::IGF SMALL BUSINESS INNOVATION RESEARCH (SBIR II) - PHYSICS BASED FAST RUNNING TOOL | $5K |
| Aug 30, 2018 | Department of DefenseW6QK ACC-APG NATICK | W911QY18C0136 | 541715 | CFD SBIR II EFFORT FOR "A MULTI-PURPOSE NOVEL BIOFIDELIC HEAD SURROGATE TO EVALUATE HEAD PROTECTION SYSTEMS FROM BALLISTIC, BLAST, AND BLUNT EXPOSURES" | $504K |
| Aug 28, 2018 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865018C5078 | 541715 | COUPLED SIMULATION TOOL FOR MODELING STRUCTURAL PROFILE DISRUPTION FOR AEROVEHICLES | $750K |
| Aug 23, 2018 | Department of DefenseW6QK ACC-RSA | W31P4Q18C0103 | 541715 | ARMY SMALL BUSINESS INNOVATION RESEARCH (SBIR) PHASE II EFFORT FOR STATEMENT OF WORK ENTITLED, "BALLISTIC MISSILE DEFENSE WEATHER MANAGEMENT" | $500K |
| Aug 22, 2018 | Department of DefenseW6QK ACC-APG DURHAM | W911NF17C0076 | 541712 | IGF::OT::IGF SBIR PHASE II | $427K |
| Aug 16, 2018 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $702K |
| Aug 13, 2018 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH18C0100 | 541715 | DHA SBIR PHASE II R&D CONTRACT FOR PROPOSAL #: H2-0343 FOR "DYNAMICS FOR WARFIGHTER AVATARS WITH COMPLETE ARTICULATED ANATOMY" | $999K |
| Aug 3, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2153 | 541715 | THE LANDING SURFACE DAMAGE AND LIBERATION OF DEBRIS PARTICLES CAUSED BY ROCKET PLUME IMPINGEMENT FLOW DURING SPACECRAFT PROPULSIVE LANDING ON UNPREPARED SURFACES OF MOON, MARS, AND OTHER CELESTIAL BODIES POSES A HIGH RISK FOR ROBOTIC AND HUMAN EXPLORATION ACTIVITIES. SIMPLY DETERMINING WHETHER THE PLUME INDUCED LOADS EXCEED THE BEDROCK BEARING CAPACITY THRESHOLD IS NOT SUFFICIENT. AN INTEGRATED MULTI-PHYSICS SIMULATION TOOL IS REQUIRED TO CAPTURE AND QUANTIFY THE ONSET, PROGRESSION AND ULTIMATE EXTENT OF THE BEDROCK FRACTURE PROCESSES AND IDENTIFY THE DANGERS OF THE RESULTING DEBRIS TRANSPORT AND LANDING SURFACE DESTRUCTION. NO SUCH SIMULATION CAPABILITY EXISTS TO DATE. CFDRC HAS TEAMED WITH THE LOS ALAMOS NATIONAL LABORATORY (LANL) TO PROPOSE THE DEVELOPMENT OF SUCH A SIMULATION TOOL THAT COMBINES STATE-OF-THE-ART COMPUTATIONAL FLUID DYNAMICS SOFTWARE FOR PLUME FLOWFIELD WITH A DYNAMIC FRACTURE MECHANICS STRUCTURAL ANALYSIS SOFTWARE OF THE ROCK MATERIAL UNDER PLUME IMPINGEMENT LOADS. THE PHASE I WILL FOCUS ON DEMONSTRATING FEASIBILITY OF THE PROPOSED APPROACH WITH A TRL OF 2 TO 3. IN PHASE II THE MODELS WILL BE EXTENDED AND VALIDATED TO PROVIDE AN ACCURATE NUMERICAL APPROACH FOR SIMULATING PLUME INDUCED ROCK FRACTURE, DEBRIS TRANSPORT AND ANALYSIS TOOL, INCREASING THE TRL BY END OF PHASE II FROM 3 TO 5. | $125K |
| Aug 3, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2154 | 541715 | SPACECRAFT PROPULSIVE LANDINGS ON UNPREPARED REGOLITH PRESENT IN EXTRA-TERRESTRIAL ENVIRONMENTS POSE A HIGH RISK FOR SPACE EXPLORATION MISSIONS. PLUME/REGOLITH INTERACTION RESULTS IN (1) THE LIBERATION OF DUST AND DEBRIS PARTICLES THAT MAY COLLIDE WITH THE LANDING VEHICLE AND (2) CRATERS WHOSE SHAPE ITSELF CAN INFLUENCE VEHICLE DYNAMICS. TO INVESTIGATE SUCH GAS-GRANULAR INTERACTIONS FOR LARGE-SCALE PROBLEMS USING STANDARD LAGRANGIAN APPROACH, PARTICLES ON THE ORDER OF BILLIONS WOULD NEED TO BE MODELLED TO ACCOUNT FOR LARGE LANDING AREAS, MAKING THE APPROACH IMPRACTICAL. AN EFFECTIVE ALTERNATIVE IS TO USE AN EULERIAN-EULERIAN APPROACH WHERE THE GRANULAR MIXTURE IS REPRESENTED USING A TWO-FLUID MODEL AND THE GRANULAR MATERIAL PHYSICS ARE CONSIDERED USING CONSTITUENT RELATIONS. THIS EFFORT AIMS TO PROVIDE A STATE-OF-THE-ART EULERIAN-EULERIAN APPROACH WITH NOVEL GRANULAR MATERIAL MODELS IN THE HIGHLY SCALABLE COMPUTATIONAL FRAMEWORK LOCI USED BY NASA ENGINEERS. AT THE END OF PHASE I, A MASSIVELY PARALLEL LOCI-BASED VERSION OF A GAS-GRANULAR FLOW SOLVER FEATURING COMPRESSIBLE FLOW, SINGLE GAS SPECIES, AND NOVEL GRANULAR MATERIAL MODELS FOR SPHERICAL AND IRREGULAR (SINGLE-COMPONENT) PARTICLE MIXTURE WILL BE DEVELOPED AND DEMONSTRATED, WITH A TRL STARTING AT 2 AND ENDING AT 4. PHASE II EFFORT WILL ADD HIGHER MODEL FIDELITY TO THE GAS PHASE WITH A MULTI-COMPONENT APPROACH, AN EXTENSION OF THE GRANULAR MODELS FOR POLY-DISPERSE MIXTURES, OVERSETMESH WITH SIX DEGREES-OF-FREEDOM FOR LANDER VEHICLE MOTION, AND COMPATIBILITY TO OTHER LOCI-BASED TOOLS AND MODULES SUCH AS CHEM. | $125K |
| Aug 3, 2018 | Department of DefenseFA9300 AFTC PZR | FA930017C2008 | 541712 | IGF::OT::IGF SMALL BUSINESS INNOVATIVE RESEARCH TECHNOLOGY TRANSITION PLAN FOR MOLECULAR DESIGN OF ENERGETIC MATERIALS | $350K |
| Aug 3, 2018 | Department of DefenseW6QK ACC-RSA | W31P4Q18P0125 | 541715 | ARMY SMALL BUSINESS INNOVATION RESEARCH (SBIR) BRIDGE GAP PURCHASE ORDER FOR WORK ENTITLED "AIR MISSILE DEFENSE WEATHER MANAGEMENT." | $50K |
| Aug 2, 2018 | 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". | $500K |
| Jul 31, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2866 | 541511 | OT: ANNUAL LEASE OF CFDACE INCLUDING CFDGEOM, CFDVIEW, MULTIPHYSICS AND STRESS MODULES AND 16 PROCESSOR PARALLEL UPGRADE. | $115K |
| Jul 27, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P1886 | 541715 | THE OVERALL OBJECTIVE OF THIS SBIR PROJECT IS THE DEVELOPMENT OF A NOVEL CONCEPT FOR LOW EMISSIONS: A LEAN FULLY PREMIXED (LFP) COMBUSTOR FOR HIGH OVERALL PRESSURE RATIO SMALL CORE ENGINES. IN ORDER TO ACHIEVE THIS MAJOR OBJECTIVE, A THREE-UNIT FULLY PREMIXED INJECTOR HAS BEEN CONCEPTUALIZED AND PROPOSED. PHASE I SCOPE INCLUDES DESIGN AND DEMONSTRATION OF THIS INJECTOR, WHICH WILL BE COMPOSED OF THREE UNITS. THE FIRST COMPONENT WILL EXECUTE COMPLETE FUEL VAPORIZATION BY HEATING FROM THE HOT COMPRESSED AIR WHILE THE SECOND COMPONENT ENSURES RAPID AND EFFICIENT PREMIXING AND THE THIRD COMPONENT GENERATES ROBUST STABILITY ASSOCIATED WITH A FULLY PREMIXED FLAME. THE ISSUES OF AUTO-IGNITION, FLASHBACK, STATIC AND DYNAMIC COMBUSTION INSTABILITIES WILL BE ADDRESSED DURING THE DESIGN OF THE LFP INJECTOR. THEORETICAL, COMPUTATIONAL, AND REDUCED-ORDER MODELING ANALYSES WILL BE UTILIZED TO DESIGN THE LFP INJECTOR DURING PHASE I. PHASE II WILL FOCUS ON THE RIGOROUS TESTING OF THIS TECHNOLOGY AS WELL AS DESIGN REFINEMENT AND OPTIMIZATION TO BE INTEGRATED WITH A RELEVANT GAS-TURBINE ENGINE. | $125K |
| Jul 27, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P1891 | 541715 | THE GOAL OF THE PROJECT IS TO DEVELOP A MATHEMATICALLY RIGOROUS, MULTI-FIDELITY SURROGATE MODELING (MFSM) METHODOLOGY TO CONSOLIDATE EXPERIMENTAL AND COMPUTATIONAL AERODYNAMIC DATA INTO INTEGRATED DATABASES WITH QUANTIFIABLE UNCERTAINTY. THE SALIENT ASPECTS OF THE PROPOSED SOLUTION ARE: (1) A HIERARCHICAL MFSM FORMULATION TO ENCAPSULATE LOCAL RESPONSE SURFACE MODELING, MODEL ADAPTATION/FUSION, INTERPOLATION/BLENDING, AND UNCERTAINTY QUANTIFICATION ONTO A HOLISTIC PLATFORM; (2) A SUITE OF SURROGATE MODELING TECHNIQUES TO CAPTURE THE LOCAL AERODYNAMIC BEHAVIOR AROUND THE OPERATING POINTS; (3) FORMAL ADAPTATION/FUSION TECHNIQUES TO BRIDGE THE GAP OF FIDELITY AND MERGE DATA FROM MULTIPLE SOURCES; (4) A GLOBAL DATA INTERPOLATION STRATEGY TO STITCH THE LOCAL MODELS FOR ACCURATE PREDICTION IN A BROAD FLIGHT PARAMETER SPACE; AND (5) A MODULAR SOFTWARE FRAMEWORK TO AUTOMATE THE PROCESS AND FACILITATE INTEGRATION WITH NASA S DATA ANALYSIS WORKFLOW. IN PHASE I, ALL KEY COMPONENTS WILL BE DESIGNED AND DEVELOPED. FEASIBILITY WILL BE DEMONSTRATED VIA CASE STUDIES OF NASA INTEREST, IN WHICH COMPUTATIONAL, WIND TUNNEL, AND FLIGHT TEST DATA WILL BE ANALYZED AND MERGED USING THE DEVELOPED SOFTWARE AND ITS PERFORMANCE (E.G., ACCURACY, RELIABILITY, DATA COMPATIBILITY, AND INTEGRABILITY) WILL BE ASSESSED. THE PHASE II EFFORT WILL FOCUS ON CAPABILITY EXTENSION, ALGORITHM OPTIMIZATION, TECHNOLOGY INTEGRATION/INSERTION, AND EXTENSIVE VALIDATION AND DEMONSTRATION. | $125K |
| Jul 27, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P1879 | 541715 | THE GOAL OF THE PROJECT IS TO DEVELOP AN INTELLIGENT FRAMEWORK TO CONSTRUCT ADAPTIVE PARAMETRIC REDUCED ORDER MODEL (PROM) DATABASE FOR AEROSERVOELASTIC (ASE) ANALYSIS AND AEROSTRUCTURAL CONTROL. LEVERAGING ON SIGNIFICANT ADVANCEMENTS BY THE PROPOSING TEAM IN PRIOR RESEARCH, THIS PHASE I EFFORT WILL INITIATE A NEW FRONTIER OF ENGINEERING INTELLIGENCE TO FURTHER ASE ROM DEVELOPMENT, INCLUDING SEVERAL EMERGING TECHNIQUES: GENETIC ALGORITHM OPTIMIZATION-GUIDED ROMS, DATA-DRIVEN ROM FOR NONLINEAR AEROELASTICITY AND GUST RESPONSE ANALYSIS, ONLINE DETERMINATION OF CRITICAL FLIGHT CONDITIONS AND IN-SITU PROM DATABASE DEVELOPMENT WHILE MODELING, CFD COMPUTATION, AND ROM ARE IN PROGRESS. A MODULAR SOFTWARE FRAMEWORK WILL BE ESTABLISHED FOR AUTOMATED PROM GENERATION AND OPTIMIZATION, CONSISTENT STATE ENFORCEMENT, ADAPTIVE PARAMETER SPACE SAMPLING, AND DATABASE POPULATION. THE FEASIBILITY OF THE PROPOSED TECHNOLOGY WILL BE DEMONSTRATED FOR ASE PROBLEMS OF NASA INTEREST (E.G., HIGH-SPEED ASE, X-56A MUTT, ETC.). THE PHASE II EFFORT WILL FOCUS ON: (1) PROM ENGINE OPTIMIZATION IN TERMS OF EXECUTION EFFICIENCY, ROBUSTNESS, AND AUTONOMY; AND (2) DIRECT INTEGRATION OF THE INTELLIGENT ENVIRONMENT INTO NASA WORKFLOW; AND PROCESS AUTOMATION OF MODELING, SIMULATION, AND CONTROL SYNTHESIS FOR TECHNOLOGY INSERTION AND TRANSITION; AND (3) EXTENSIVE SOFTWARE VALIDATION AND DEMONSTRATION FOR ASE AND FLIGHT CONTROL ANALYSIS OF REALISTIC AIRCRAFTS OF CURRENT NASA INTEREST | $125K |
| Jul 18, 2018 | Department of DefenseW6QK ACC-APG ADELPHI | W911QX18P0180 | 541715 | 6 MONTH SBIR PHASE 1 TOPIC A18-034. THE CONTRACTOR SHALL DELIVER AN INTEGRATED PLUG-AND-PLAY (PNP) TOOL/PLATFORM BASED ON NEURAL NETWORK MODELS FOR REAL-TIME MONITORING, PROGNOSTICS, AND CONTROL OF MECHANICAL SYSTEMS. | $100K |
| Jul 17, 2018 | Department of DefenseFA9453 AFRL RVK | FA945318P0238 | 541715 | IGF::OT::IGF CARBON NANOTUBE - COPPER COMPOSITE AS ELECTRON EMITTER FOR PASSIVE SPACECRAFT DISCHARG | $150K |
| Jul 12, 2018 | Department of CommerceDEPT OF COMMERCE NOAA | 1305M218CNRMW0045 | 541715 | THIS AWARD IS FOR THE SMALL BUSINESS INNOVATION RESEARCH (SBIR) PHASE I FOR FY2018'S PROGRAM ANNOUNCEMENT FOR THE TECHNOLOGY PARTNERSHIPS OFFICE UNDER THE OFFICE OF ATMOSPHERIC RESEARCH IN SILVER SPRING, MD. THIS AWARD IS FOR PROPOSAL 18-1-048 A PROJECT TITLED "A LOCATION-BASED WEATHER THREAT TRACKING AND NOTIFICATION SYSTEM." | $120K |
| Jul 11, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833517C0400 | 541712 | RESEARCH AND DEVELOPMENT IGF::OT::IGF | $100K |
| Jun 28, 2018 | Department of DefenseFA9101 AEDC PKP PROCRMNT BR | FA910118P0046 | 541715 | SMALL BUSINESS INOVATION RESEARCH PHASE 1 - DEVELOPMENT OF GEOMETRY KERNEL FOR DYNAMIC SIMULATIONS | $150K |
| Jun 14, 2018 | 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. | $370K |
| Jun 5, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0054 | 541715 | COMPUTATIONAL FLUID DYNAMICS (CFD) TECHNOLOGY PLAYS A STRONG ROLE IN THE DESIGN AND DEVELOPMENT OF AEROSPACE AND DEFENSE VEHICLES SUCH AS HIGH-SPEED APPLICATIONS WHERE TESTING UNDER THE CORRECT OPERATIONAL CONDITIONS IS NOT YET VIABLE. DESPITE DECADES OF RESEARCH TOWARDS MAKING CFD PREDICTIVE AND RELIABLE, IT HAS NOT PROVEN SO DUE TO THE SIGNIFICANT UNCERTAINTIES IN PHYSICAL MODELS, INITIAL/BOUNDARY CONDITIONS, COMPUTATIONAL MESH, NUMERICAL SCHEMES AND METHODS. IN THE PROPOSED EFFORT CFDRC IN PARTNERSHIP WITH VIRGINIA TECH AND UTSI, AIMS TO DIRECTLY ADDRESS THESE ISSUES BY INTEGRATING DIMENSIONALLY ADAPTIVE SPARSE GRID UNCERTAINTY QUANTIFICATION (UQ) METHOD WITH AN EXISTING REACTING CFD SOLVER. THE PROPOSERS DEMONSTRATED THIS APPROACH TO BE SUITABLE FOR ACHIEVING THIS OBJECTIVE DURING PHASE I ON A NASA-LARC NOZZLE-ISOLATOR LAB-SCALE SETUP. THE PROPOSED EFFORT WILL DELIVER A PRACTICAL USER-FRIENDLY AUTOMATED SOFTWARE TOOL COMBINING UQ WITH CFD (UQCFD), CAPABLE OF IDENTIFYING AND CHARACTERIZING REGIONS OF HIGH-UNCERTAINTY IN THE CFD CODE AND THE ASSOCIATED WORK-FLOW, AND THEREBY, PROVIDE GUIDANCE TO THE CFD MODELER TO INCREASE FIDELITY OF THOSE REGIONS. UQCFD SOFTWARE HAS THE POTENTIAL TO MAKE SIGNIFICANT IMPACT ON A WIDE VARIETY OF APPLICATION UTILIZING CFD PREDICTIONS INCLUDING DESIGN AND DEVELOPMENT OF NEXT GENERATION SUPERSONIC AND HYPERSONIC FLIGHT VEHICLES. | $750K |
| May 24, 2018 | Department of DefenseW6QK ACC-RSA | 0001 | 541712 | IGF::CT::IGF | $1.1M |
| May 1, 2018 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014718C7329 | 541715 | SBIR/STTR PHASE II R&D FINE POWDER CATHODE AND SEPARATOR BINDER CHARACTERIZATION FOR THERMAL BATTERIES | $993K |
| Apr 30, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0053 | 541715 | 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 DEVELOP A PHYSICS BASED MODEL OF AN EBC SYSTEM INTERACTING WITH THE FLOW ENVIRONMENT TO PROVIDE BETTER UNDERSTANDING OF THE DYNAMIC PROCESSES THAT EFFECT EBC DURABILITY UNDER PROPULSION CONDITIONS. THE MODEL USES COMPUTATIONAL FLUID DYNAMICS TO ESTABLISH THE CONDITIONS AND SPECIES CONCENTRATIONS ACROSS THE SURFACE OF THE STRUCTURE. THE RESPONSE WITHIN THE COATING TO THE ENVIRONMENTS IS PREDICTED USING MICROSCALE SIMULATIONS WHERE EACH COMPONENT OF THE COMPOSITE COATING SYSTEM IS DISCRETELY RESOLVED. THE MICROMECHANICS MODELS ARE BASED ON PERIDYNAMICS, A MESH FREE THEORY OF CONTINUUM MECHANICS THAT SIMULTANEOUSLY SOLVES FOR THERMAL, MECHANICAL AND CONCENTRATION GRADIENTS COUPLED WITH DAMAGE TO THE MATERIAL. RESULTS OF NUMEROUS MICROSCALE SIMULATIONS ARE USED TO INFORM A TIME, TEMPERATURE AND STRESS BASED DAMAGE CRITERIA FOR A HOMOGENIZED COATING MATERIAL WHICH IN TURN CAN BE USED TO PREDICT THE EXTENT OF COATING BREAK DOWN AND MASS LOSS AT EACH INTEGRATION POINT WITHIN BOUNDARY OF A CFD SIMULATION. | $750K |
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