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CASCADE TECHNOLOGIES INC
UEI: K9KCLNBFQAF6
# of Employees: 12
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Phase Transitions, Nucleation and Mixing Modeling through Trans-Critical Conditions
Amount: $149,999.00ABSTRACT: In this proposal, researchers from Cascade Technologies and Professors Matthias Ihme and Ali Mani from Stanford University lay out a plan to develop predictive modeling tools for transcriti ...
STTRPhase I2015Department of Defense Air Force -
Web platform architecture for CFD simulations and real-time analysis on HPC resources
Amount: $150,000.00The availability and continued growth of High Performance Computing (HPC) is opening new avenues for complex physics based software simulations. The usage of HPC is particularly important in high-fid ...
SBIRPhase I2014Department of Energy -
Tactical Airplane Noise Reduction via Advanced Automated Computational Airframe Aft-End Integration Technologies
Amount: $149,999.00Cascade Technologies and its collaborators from Stanford University propose to develop an efficient and robust computational framework to optimize the aerodynamic interactions between vortices shed by ...
SBIRPhase I2014Department of Defense Navy -
Design Optimization and Analysis of Advanced Exhaust Systems
Amount: $80,000.00Cascade Technologies and its collaborators from the Florida State University and Stanford University propose to develop a robust computational framework to enable geometrical optimization of complex n ...
STTRPhase I2014Department of Defense Navy -
Modeling of interior nozzle flows for transient effects, realistic high performance nozzle physics and coupling to Large Eddy Simulation modeling of t
Amount: $149,995.00The 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 I2013Department of Defense Navy -
Turbulent Combustion Interaction Models for LES Simulations of High Speed Flow
Amount: $749,975.00This work will develop and validate a high-fidelity LES combustion model based on Flamelet Progress Variable approach for accurate prediction of high-speed turbulent combustion. The flamelet-modeling ...
STTRPhase II2012Department of Defense Air Force -
Turbulent Combustion Interaction Models for LES Simulations of High Speed Flow
Amount: $100,000.00At present, the predictive capability of simulation codes and models used in the conceptual planning and design of high-speed propulsion systems is limited by the ability to describe the complex flow ...
STTRPhase I2011Department of Defense Air Force -
Heat Transfer Prediction in Transitional Hypersonic Flow
Amount: $750,000.00ABSTRACT: Predicting the wall heat loading experienced by hypersonic vehicles during the transition from laminar to turbulent boundary layer flow is the grand-challenge tackled by the present proposa ...
STTRPhase II2011Department of Defense Air Force -
Large Eddy Simulations of Hot Supersonic Jets for Aeroacoustics
Amount: $744,193.00LES will be used to calculate flow and noise issuing from realistic engine configurations such as realistic engine nozzle throats, serrated nozzles, straight ramp diffusers, and over/under expanded op ...
STTRPhase II2011Department of Defense Navy -
Real-Time Simulation Methodology for Rotor-Airwake Interactions
Amount: $80,000.00The overall objective of this proposal is to develop a physics based methodology that is capable of simulating two-way coupled, non-linear interaction of ship-airwake and helicopter rotor-wake in flow ...
SBIRPhase I2011Department of Defense Navy
