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SBC: CFD RESEARCH CORPORATION Topic: MDA14T002
Thermally induced fatigue and residual stress introduced during fabrication are sources of failure in microelectronics, which raises reliability concerns for MDA and its system integrators. CFDRC has teamed with experts in the reliability of microelectronics packaging to develop a physics based modeling and testing protocol to correlate material properties and thermal loading conditions to stress ...STTR Phase II 2016 Department of DefenseMissile Defense Agency
SBC: CFD RESEARCH CORPORATION Topic: A17AT022
The overall objective of this project (Phase I, II, and III) is to develop, fabricate, and test a novel biofidelic rat surrogate for the validation of primary blast loading conditions for mild traumatic brain injury (mTBI). The CFDRC/NJIT team will use extensive knowledge of blast loading characteristics and TBI studies coupled with past/ongoing efforts designing and testing a rat surrogate. In P ...STTR Phase I 2017 Department of DefenseArmy
Extending Molecular Simulation to Grain Scale for Simulating Response of Energetic Material Under High Strain Rate and Shock LoadingSBC: CFD RESEARCH CORPORATION Topic: AF17AT023
High Velocity Penetrator Weapons experience severe stress in terms of high frequency vibration and shock during launch, flight, and on impact. The extreme conditions have significant impact on the survivability of the weapon due to damage of the energetic material and fuze compartment. Molecular dynamics is often used to understand the effect of external shock on the material. However, molecular ...STTR Phase I 2017 Department of DefenseAir Force
SBC: CFD RESEARCH CORPORATION Topic: AF17AT025
High speed air vehicles, already operating at material strength performance limits, are at significant risk when subjected to additional localized heating from sources such as directed energy. This localized heating may result in material softening, pitting and burn through causing structural damage and alteration of the structural profile. This damage can disrupt the aerodynamic performance and ...STTR Phase I 2017 Department of DefenseAir Force
SBC: CFD RESEARCH CORPORATION Topic: AF16AT14
The objective of the proposed Phase II effort is to establish fundamental understanding of combustion-physical mechanisms leading to blowout, the critical evaluation of model limitations in predicting these blowout processes and the development of an improved combustion model to enable the prediction of lean blowout (LBO) in swirl-stabilized combustors. For this, high-resolution numerical simulati ...STTR Phase II 2017 Department of DefenseAir Force
SBC: CFD RESEARCH CORPORATION Topic: DTRA16A003
Cost-effective application of advanced commercial electronics technologies in DoD space systems requires early development of radiation-hardened-by-design (RHBD) techniques, and use of simulations is critical to the efficiency of this process. CFDRC has developed an integrated, mixed-mode simulation approach allowing their NanoTCAD device physics simulator to interface with commercial circuit simu ...STTR Phase I 2017 Department of DefenseDefense Threat Reduction Agency
SBC: CFD RESEARCH CORPORATION Topic: MDA16T001
Fine powder thermal battery cathode materials can exhibit challenging flow properties which makes processing with automated presses difficult.Granulating these powders substantially improves flow properties and reduces the tendency for powder segregation during handling and pressing operations.The properties of Magnesium Oxide (MgO) that lead to good performance in thermal battery separators are n ...STTR Phase I 2017 Department of DefenseMissile Defense Agency
Physics-based Computationally Efficient Spray Combustion Models for LES of Multiphase Reacting FlowsSBC: CFD RESEARCH CORPORATION Topic: N17AT002
One important challenge for the reliable prediction of liquid fuel effects on the combustion in aviation combustors and augmentors is the accurate modeling of underlying physical processes, involving the evaporation of fuels, preferential vaporization, scalar mixing and ignition. LES methodologies are required to accurately capture these transient and inherently unsteady combustion processes. In t ...STTR Phase I 2017 Department of DefenseNavy
Computationally Efficient, Accurate and Uncertainty Characterized Chemical Kinetics for Hydrocarbon FuelsSBC: CFD RESEARCH CORPORATION Topic: AF17AT004
TBDSTTR Phase I 2017 Department of DefenseAir Force
SBC: CFD RESEARCH CORPORATION Topic: AF16AT14
Next-generation turbulent combustion models must enable accurate prediction of lean blow-out and flashback for complex geometries, fuels and operating conditions relevant to the Air Force. Improved models are needed to better predict kinetically and hydr...STTR Phase I 2016 Department of DefenseAir Force