You are here
CASCADE TECHNOLOGIES INC
UEI: K9KCLNBFQAF6
# of Employees: 12
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
-
Highly scalable large-eddy simulations of oxy-fuel combustors for direct-fired supercritical CO2 power cycles
Amount: $999,989.00Direct-fired supercritical CO2 cycles are an emerging energy conversion technology that promises to increase power plant efficiency while capturing all CO2 emissions. However, given the novelty of the ...
SBIRPhase II2018Department of Energy -
Fast, Parallel, High-Quality Voronoi Mesh Generator
Amount: $124,704.00In this work we propose to further develop and demonstrate a mesh generation approach based on clipped Voronoi diagrams. This approach to mesh generation has the potential to significantly improve per ...
SBIRPhase I2018National Aeronautics and Space Administration -
Prediction and Modal Analysis of Supersonic Jet Noise From Complex Nozzles in an Integrated Simulation Environment
Amount: $124,733.00Our long-term vision is to seamlessly integrate resolvent operator-based spectral analysis into Cascade’s high-fidelity large eddy simulation (LES) environment, for accurate prediction and efficient ...
SBIRPhase I2018National Aeronautics and Space Administration -
Highly Scalable Large-eddy Simulations of Oxy-fuel Combustors for Direct-fired Supercritical CO2 Power Cycles
Amount: $154,184.00The safety, reliability and efficiency of direct-fired sCO2 cycles depend to a large extent upon the combustor performance. However, multi-scale interactions between turbulence and chemistry remain an ...
SBIRPhase I2017Department of Energy -
Machine-Learning & QMU for Multi-Fidelity Analysis of Scramjet Operability
Amount: $124,941.00Dual-mode scramjets have the potential to operate efficiently in a variety of flight conditions without requiring complicated variable configurations, thus providing cost-effective access to space and ...
SBIRPhase I2017National Aeronautics and Space Administration -
A Massively Parallel Framework for Low-Dissipation, Multiphysics Simulations of Rocket Engines
Amount: $124,952.00In this proposal, researchers from Cascade Technologies and Stanford University outline a multi-year research plan to develop large-eddy simulation (LES) tools to predict and understand combustion ins ...
STTRPhase I2017National Aeronautics and Space Administration -
High-Fidelity Design Tools and Technologies for High-Pressure Heavy Fuel Injectors
Amount: $149,938.83The objective of the proposed SBIR project is to develop a computational tool capable of predicting the atomization of liquid injected through a practical I.C. Engine fuel injector under realistic ope ...
SBIRPhase I2017Department of Defense Army -
Modeling of interior nozzle flows for transient effects, realistic high performance nozzle physics and coupling to Large Eddy Simulation modeling of t
Amount: $2,048,271.00The objective of the present proposal is to develop and apply accurate, robust and cost-effective methodologies for the prediction of the interior nozzle flow, seamlessly coupled with high-fidelity la ...
SBIRPhase II2016Department of Defense Navy -
Tactical Airplane Noise Reduction via Advanced Automated Computational Airframe Aft-End Integration Technologies
Amount: $996,578.00The objective of the present technical effort is to analyze and design noise-reduction devices and shape modifications of the airframe aft-end to tailor its interaction with the jet as a mechanism to ...
SBIRPhase II2016Department of Defense Navy -
Web platform architecture for CFD simulations and real-time analysis on HPC resources
Amount: $999,998.00The availability and continued growth of high performance computing (HPC) is opening new avenues for complex physics based software simulations. The usage of high performance computing is particularly ...
SBIRPhase II2015Department of Energy
