CASCADE TECHNOLOGIES, INC.

Company Information
Address 2445 FABER PL STE 100
PALO ALTO, CA, 94303-3347

http://www.cascadetechnologies.com

Information

DUNS: 179576715

# of Employees: 11


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Highly Scalable Large-eddy Simulations of Oxy-fuel Combustors for Direct-fired Supercritical CO2 Power Cycles

    Amount: $154,184.00

    The 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
  2. Modeling of interior nozzle flows for transient effects, realistic high performance nozzle physics and coupling to Large Eddy Simulation modeling of t

    Amount: $749,293.00

    The 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
  3. Phase Transitions, Nucleation and Mixing Modeling through Trans-Critical Conditions

    Amount: $149,999.00

    ABSTRACT: 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
  4. Tactical Airplane Noise Reduction via Advanced Automated Computational Airframe Aft-End Integration Technologies

    Amount: $748,027.00

    The 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 II2015Department of Defense Navy
  5. Web platform architecture for CFD simulations and real-time analysis on HPC resources

    Amount: $999,998.00

    The 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
  6. Tactical Airplane Noise Reduction via Advanced Automated Computational Airframe Aft-End Integration Technologies

    Amount: $149,999.00

    Cascade 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
  7. Design Optimization and Analysis of Advanced Exhaust Systems

    Amount: $80,000.00

    Cascade 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 I2014Navy Department of Defense
  8. Web platform architecture for CFD simulations and real-time analysis on HPC resources

    Amount: $150,000.00

    The 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
  9. Modeling of interior nozzle flows for transient effects, realistic high performance nozzle physics and coupling to Large Eddy Simulation modeling of t

    Amount: $149,995.00

    The 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
  10. Turbulent Combustion Interaction Models for LES Simulations of High Speed Flow

    Amount: $749,975.00

    This 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

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