Award Data

Conventional air-vehicle designs are subjected to a well-set system/operational requirements. Scramjet-powered vehicle (SPV) design however enters an unprecedented level of multidisciplinary synergy to achieve its operational requirements. Through a convoluted and inverse design strategy for SPV, its propulsion system inlet design largely dictates the airframe geometry. Further, it is complicated ...

The overall objective of the proposed Phase II STTR program is to continue optimization of properties already obtained during Phase I which established the feasibility of concept to multi-functionality for BMI polymer matrix composites along with structural capability. Throughout this 2-year effort, it is proposed to seek optimization of the composite properties. The goal is develop and demonstrat ...

Cermet, Inc in collaboration with Georgia Institute of Technology proposes to develop spin Light Emitting Diode (LED) in a 24 month Phase II program. The spin LED is a simple yet powerful spintronic device that produces circularly polarized light and is a potent tool to quantify the spin injection efficiency and spin polarization efficiency.

An increasing amount of information comes in the form of streaming text: news media, email, and even human conversation. Creating insight from streaming text has been challenging though, because current knowledge discovery systems depend on expert analysts to move from simple data to actionable knowledge. In order for such systems to be used outside a small cadre of experts, they must incorporat ...

nGimat Co., in collaboration with the Georgia Institute of Technology, and the Wright-Patterson AFB Air Force Research Laboratory, proposes to develop a fuel injection method and advanced numerical simulation tools for injection of fuel at supercritical conditions in aero-propulsion combustors. This project is designed to accelerate understanding and commercialization of transcritical and supercr ...

Combustion powered actuation (COMPACT) is a flow control technology developed at Georgia Tech which utilizes a miniature combustion chamber (cubic centimeter scale) to produce high-speed pulsed jets suitable for aerodynamic flow control (separation control, drag reduction, shock control, etc.) at transonic or supersonic speeds. The system is lightweight, can be operated with passive fluidic valve ...