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CASCADE TECHNOLOGIES INC

Company Information
Address
1072 E MEADOW CIR
PALO ALTO, CA 94303-4230
United States


http://www.cascadetechnologies.com

Information

UEI: K9KCLNBFQAF6

# of Employees: 12


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Computational Characterization of Aeroengine Combustor/Augmentor Fuel Injectors

    Amount: $999,985.00

    The work proposed for this project arises from the need for modeling a realistic fuel atomization process in a complex combustor/augmentor fuel injector. In a real gas turbine combustor or augmentor, ...

    SBIRPhase II2011Department of Defense Navy
  2. Towards More Efficient Comprehensive Rotor Noise Simulation

    Amount: $100,000.00

    Rotorcraft design and optimization currently still rely largely on simplified (low-fidelity) models, such as rotor disk or wake models to reduce the turn-around time and allow exploration of a large p ...

    SBIRPhase I2010National Aeronautics and Space Administration
  3. Effect of Engine Installation on Jet Noise using a Hybrid LES/RANS Approach

    Amount: $100,000.00

    Installation effects arising from propulsion airframe interaction are known to produce substantial variations in the in-situ jet noise. A hybrid LES/RANS computational framework is proposed for predic ...

    SBIRPhase I2010National Aeronautics and Space Administration
  4. Efficient Implementation of Models for Improved Prediction of Gas Turbine Combustor and Augmentor Robustness

    Amount: $100,000.00

    Sophisticated models will be developed for accurate simulation of gas turbine combustion occurring in the augmentor regions of modern military aircraft engines. The focus will be on the formulation of ...

    SBIRPhase I2010Department of Defense Air Force
  5. Aeroacoustics of High-Speed Jet Impingement

    Amount: $80,000.00

    CASCADE Technologies is proposing to use CharLES, its in-house unstructured large eddy simulation technology (LES), to simulate the flow and noise emitted from supersonic impinging jets. This problem ...

    SBIRPhase I2010Department of Defense Navy
  6. Computational Characterization of Aeroengine Combustor/Augmentor Fuel Injectors

    Amount: $149,986.00

    Liquid fuel injected into combustors has to undergo atomization in order to increase the available fuel surface area for fast evaporation, mixing, and subsequent combustion. Experimental access to the ...

    SBIRPhase I2010Department of Defense Navy
  7. Large Eddy Simulations of Hot Supersonic Jets for Aeroacoustics

    Amount: $70,000.00

    The technical objective of this proposal is to develop and demonstrate LES capability to predict hot jet noise at supersonic operating conditions of tactical aircrafts. We also propose an LES based no ...

    STTRPhase I2009Department of Defense Navy
  8. Heat Transfer Prediction in Transitional Hypersonic Flow

    Amount: $100,000.00

    Accurate prediction of heat transfer in hypersonic boundary layers undergoing transition from laminar to turbulent regime is a technical challenge. Heat transfer overshoot at transition region is of p ...

    STTRPhase I2009Department of Defense Air Force
  9. Rotor Wake Computations for Direct Integration with Current CFD Technology

    Amount: $70,000.00

    The technical objective is to develop methodology and tools suitable for the integration of more efficient but accurate rotor wake computations within current unstructured CFD computations. The propos ...

    STTRPhase I2009Department of Defense Navy
  10. Efficient Kinetic/Continuum Simulations of Hypervelocity Gas Flows in Nonequilibrium Dissociation and Ionization for Earth Atmospheres

    Amount: $99,976.00

    In this project, we propose an original method to simulate dissociated and ionized hypersonic air flows from continuum to rarefied regimes for a wide range of scales inherent in Air Force applications ...

    STTRPhase I2009Department of Defense Air Force
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