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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
SBC: METACOMP TECHNOLOGIES INC Topic: AF16AT14
The ability of Large-eddy simulation (LES) techniques to accurately predict combustion instabilities and the onset of lean blow-out is not yet firmly established, especially in realistic operating conditions. A number of modeling choices play an importan...STTR Phase I 2016 Department of DefenseAir Force
SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP Topic: AF16AT16
Future gas turbine propulsion designs, in addition to incorporating variable geometrical engine features, will require controlling and integrating large power generation/extraction, as well as, managing thermal limits of the components. The engine contro...STTR Phase I 2016 Department of DefenseAir Force
Intelligent and Multiplexable Ultra-High-Temperature Fiber-Optic Pressure Sensors for Robust Distributed Engine ControlSBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP Topic: AF16AT18
Next-generation intelligent engines will operate at higher temperatures for increased efficiency and will migrate from centralized to distributed control. There is critical need for sensors for operation at ultra-high temperatures (3000F). Conven...STTR Phase I 2016 Department of DefenseAir Force
Validation Experiments to Measure Transient Aerothermoelastic Response of a Curved Panel to Hypersonic FlowsSBC: METROLASER, INCORPORATED Topic: AF16AT24
An experiment to obtain validation data on the transient aerothermoelastic response of a curved panel in hypersonic flows will be designed and evaluated for its feasibility. Significant challenges must be overcome for a successful experimental campaign i...STTR Phase I 2016 Department of DefenseAir Force
SBC: GLOBAL AEROSPACE CORPORATION Topic: AF16AT24
The Air Force is interested in developing technology that would enable long duration hypersonic flight with reusable aircraft. Hypersonic flow presents many design challenges that can be encapsulated into an aerothermoelastic problem, i.e., a complex dyn...STTR Phase I 2016 Department of DefenseAir Force
SBC: GRAMMATECH INC Topic: AF16AT19
GrammaTech proposes WARP, a tool for Weaving Application-specific Runtime Policies into embedded systems binaries.Perimeter defenses such as firewalls or network filters provide insufficient security and generic inline defenses such as control flow or ...STTR Phase I 2016 Department of DefenseAir Force
SBC: J.T. McGraw and Associates, LLC Topic: AF16AT05
Commercially-derived telescope systems, consisting mostly of commercially available components assembled to optimally meet space surveillance goals, stand ready to temporarily replace, supplement and/or augment existing optical surveillance systems. In t...STTR Phase I 2016 Department of DefenseAir Force
SBC: EXOANALYTIC SOLUTIONS INC Topic: AF16AT05
ExoAnalytic Solutions, teamed with Texas A&M University, will develop Highly-mobile Autonomous Rapidly Relocatable Integrated Electro-optical Resources (HARRIER) with the goal being to design and demonstrate tracking of resident space objects (RSOs) in n...STTR Phase I 2016 Department of DefenseAir Force
SBC: METROLASER, INCORPORATED Topic: AF16AT06
A diagnostic is proposed for obtaining instantaneous three-dimensional volumetric distributions of density in a flow field at velocities ranging from subsonic to supersonic. Two variants of laser-based Rayleigh scattering will be investigated, each of wh...STTR Phase I 2016 Department of DefenseAir Force