Cascade TechNologies, Inc.

Company Information

Company Name
Cascade TechNologies, Inc.
Address
2445 Faber Place
Suite 100
Palo Alto, CA, 94303-3347
Phone
1 650-224-4882
URL
http://www.cascadetechnologies.com
DUNS
179576715
Number of Employees
12
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$1,099,859.00
12
SBIR Phase II
$2,700,120.00
3
STTR Phase I
$619,751.00
7
STTR Phase II
$2,983,901.00
4

Award List

  1. 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 ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  2. 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 ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  3. 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 ...

    SBIR Phase I 2010 Air ForceDepartment of Defense
  4. 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 ...

    SBIR Phase I 2010 NavyDepartment of Defense
  5. Computational Characterization of Aeroengine Combustor/Augmentor Fuel Injectors

    Amount: $80,000.00

    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 ...

    SBIR Phase I 2010 NavyDepartment of Defense
  6. High Fuel-to-Air Ratio (FAR) Development Tool

    Amount: $69,995.00

    The objective of this proposal is to develop a simulation tool capable of accurate predictions of the complex mixing process in gas turbine engine combustors, applicable to complex geometry, multi-phy ...

    SBIR Phase I 2004 NavyDepartment of Defense
  7. High Fuel-to-Air Ratio (FAR) Development Tool

    Amount: $948,714.00

    The objective is to develop a simulation tool capable of accurate predictions of the complex mixing process in gas turbine engine combustors, applicable to complex geometry, multi-physics problems, an ...

    SBIR Phase II 2005 NavyDepartment of Defense
  8. Advanced Liquid Surface Tracking Software for Predicting Atomization in Gas Turbine Combustors and Augmentors

    Amount: $79,958.00

    The atomization of liquid fuels is a key process in gas turbine engines and augmentors, directly influencing combustion and thus engine performance. While adequate models exist for the secondary atomi ...

    SBIR Phase I 2007 NavyDepartment of Defense
  9. Flame Ignition/Extinction Model for Static Stability Prediction

    Amount: $99,911.00

    Ensuring static stability of the flame is of utmost importance in augmentor systems. It is proposed to develop an optimum set of models that will numerically simulate turbulent combustion in augmentor ...

    SBIR Phase I 2007 Air ForceDepartment of Defense
  10. Stability Models for Augmentor Design Tools and Technology Assessment

    Amount: $99,775.00

    We are proposing a joint experimental/modeling and computational study to develop stability models for CFD codes to design advanced augmentors. Experiments will be conducted at the Research Institutio ...

    STTR Phase I 2007 Air ForceDepartment of Defense

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