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CONTINUUM DYNAMICS INC
UEI: DUE3E75K1MJ3
# of Employees: 26
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Hardening Advanced Methods for Predicting 3D Unsteady Flows Around Wind Turbines for Industrial Use
Amount: $149,923.00Wind power plays an increasingly important role in satisfying the power needs of the U.S., and serves to reduce dependence on fossil fuels. With increased penetration, significant maintenance costs a ...
STTRPhase I2015Department of Energy -
Virtual Visual Landing Aid for Rotorcraft Recovery (V2LAR2)
Amount: $79,991.00Operational utility for ship-based rotorcraft is often limited by weather conditions that can influence sea states, wind over deck (WOD) and airwake turbulence, and pilot visibility. Recent advances i ...
SBIRPhase I2014Department of Defense Navy -
Low-Cost CFD-Based Analysis for Surface Mesh Interrogation and Refinement
Amount: $999,299.00Accurate flow calculation is crucial to the development and support of air platforms, and CFD has been successful at predicting aerodynamic performance for a variety of flows. The accuracy of CFD is ...
SBIRPhase II2014Department of Defense Army -
Small VTOL UAV Acoustics Measurement and Prediction
Amount: $124,958.00Interest in civilian use of small Unmanned Aerial Vehicles (UAVs) with Vertical Takeoff and Landing (VTOL) capability has increased greatly in recent years, and is expected to grow significantly in th ...
SBIRPhase I2014National Aeronautics and Space Administration -
Variable-Fidelity Aeroservoelastic Analysis Tool for Concept Evaluation, Design and Wind-Tunnel Test Support
Amount: $124,896.00Ongoing work in advanced air-vehicles, such as ultra-light-weight truss-braced and elastically tailored concepts is beginning to provide the insight necessary to meet NASA's N+3 transport system goals ...
SBIRPhase I2014National Aeronautics and Space Administration -
Camber Configuration Control for Performance Optimization (C3PO)
Amount: $124,711.00A novel actuation concept previously used for trailing edge tab control is to be extended for use in spanwise camber control for enhanced aerodynamic performance of next generation aircraft designs. ...
SBIRPhase I2014National Aeronautics and Space Administration -
Creating Spatial Disorientation in Flight Simulation
Amount: $149,772.23Training in the symptoms of Spatial Disorientation (SD) has shown to be valuable in aiding pilots to recognize its onset and provide a means for mitigating its effects, but such demonstrations have tr ...
SBIRPhase I2013Department of Transportation -
Adaptive Nozzle Technology for Mitigation of High Speed Jet Exhaust Noise
Amount: $728,890.00ABSTRACT: Current generation engines for Air Force platforms provide unprecedented levels of thrust and performance but also generate significantly higher jet exhaust noise than legacy tactical aircr ...
SBIRPhase II2013Department of Defense Air Force -
High-Order Aeromechanics Model Support for Rotorcraft Conceptual Design
Amount: $124,976.00Conceptual design tools for rotorcraft are used to size vehicles for intended flight operations, as well as reveal trends on the relative benefits certain configuration choices have on the resulting a ...
SBIRPhase I2013National Aeronautics and Space Administration -
Low-Cost CFD-Based Analysis for Surface Mesh Interrogation and Refinement
Amount: $99,954.00Accurate flow calculation is crucial to the development and support of air platforms, and CFD has been successful at predicting aerodynamic performance for a variety of flows. The accuracy of CFD is g ...
SBIRPhase I2013Department of Defense Army
