CASCADE TECHNOLOGIES, INC.

Basic Information

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

http://www.cascadetechnologies.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 179576715
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 11


  1. 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 ...

    SBIR Phase II 2015 Department of Energy
  2. 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 ...

    SBIR Phase I 2014 Department of Energy
  3. 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 ...

    SBIR Phase I 2014 Department of Defense Navy
  4. 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 ...

    STTR Phase I 2014 Navy Department of Defense
  5. 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 ...

    SBIR Phase I 2013 Department of Defense Navy
  6. 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 ...

    STTR Phase II 2012 Department of Defense Air Force
  7. Turbulent Combustion Interaction Models for LES Simulations of High Speed Flow

    Amount: $100,000.00

    At 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 ...

    STTR Phase I 2011 Department of Defense Air Force
  8. Heat Transfer Prediction in Transitional Hypersonic Flow

    Amount: $750,000.00

    ABSTRACT: 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 ...

    STTR Phase II 2011 Air Force Department of Defense
  9. Large Eddy Simulations of Hot Supersonic Jets for Aeroacoustics

    Amount: $744,193.00

    LES 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 ...

    STTR Phase II 2011 Navy Department of Defense
  10. Real-Time Simulation Methodology for Rotor-Airwake Interactions

    Amount: $80,000.00

    The 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 ...

    SBIR Phase I 2011 Department of Defense Navy

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