Comet Technology Corporation

Company Information
Address MI
Ann Arbor, MI, 48108-8593

http://www.cometacoustics.com

Information

DUNS: 136770703

# of Employees: 4


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: Y

Woman Owned: N



Award Charts




Award Listing

  1. Substrucured, Meshless and Parametric Modeling of Vibroacoustic Systems

    Amount: $124,843.00

    Aerospace structures are often subjected to a broad spectrum of mechanical and/or aerodynamic excitations and, therefore, there is a real need for the development of a modeling technique which can be ...

    SBIRPhase I2013National Aeronautics and Space Administration
  2. Hybrid Element Method for Compsoite Structures Subjected to Boundary Layer Loading

    Amount: $98,183.00

    In many situations, aerospace structures are subjected to a wide frequency spectrum of mechanical and/or acoustic excitations and therefore, there is a need for the development of numerical modeling t ...

    SBIRPhase I2011National Aeronautics and Space Administration
  3. Failure Initiation Predictors for Reliability-Based Design of Hybrid Composite Materials

    Amount: $749,452.00

    ABSTRACT: This proposal is concerned with the development of a novel failure initiation and progressive failure analysis modeling method for advanced composite structures, including the analysis of s ...

    STTRPhase II2010Air Force Department of Defense
  4. Hybrid Element Method for Mid-Frequency Vibroacoustic Analysis

    Amount: $99,930.00

    In many situations, aerospace structures are subjected to a wide frequency spectrum of mechanical and/or acoustic excitations and therefore, there is a need for the development of numerical modeling t ...

    SBIRPhase I2009National Aeronautics and Space Administration
  5. Failure Initiation Predictors for Reliability-Based Design of Hybrid Composite Materials

    Amount: $99,719.00

    This proposal is concerned with the development of a novel failure initiation and progressive failure analysis (PFA) modeling method for advanced composite structures. The laminate is modeled as a col ...

    STTRPhase I2009Air Force Department of Defense
  6. Identification and Reduction of Turbomachinery Noise

    Amount: $599,647.00

    Communities near airports are often exposed to high noise levels due to low flying aircraft in the takeoff and landing phases of flight. Propulsion source noise is the major contributor to the overall ...

    SBIRPhase II2007National Aeronautics and Space Administration
  7. Identification and Reduction of Turbomachinery Noise

    Amount: $69,272.00

    Noise has become a primary consideration in the design and development of many products, particulary in aerospace, automotive and consumer product industries. Communities near airports are often expos ...

    SBIRPhase I2006National Aeronautics and Space Administration
  8. Vehicle Interior Noise Prediction Using Energy Finite Element Analysis

    Amount: $598,182.00

    It is proposed to develop and implement a computational technique based on Energy Finite Element Analysis (EFEA) for interior noise prediction of advanced aerospace vehicles that will expand NASA's no ...

    SBIRPhase II2005National Aeronautics and Space Administration
  9. Vehicle Interior Noise Prediction Using Energy Finite Element Analysis

    Amount: $69,800.00

    Prediction and enhancement of vehicle interior noise due to high frequency excitation, based on computer simulation, allows the application of the technology at the early stage of design process there ...

    SBIRPhase I2004National Aeronautics and Space Administration
  10. Identification of Turbomachinery Noise Sources Using Acoustical Holography

    Amount: $69,752.00

    Evaluation and enhancement of the acoustical performance of turbomachinery requires knowledge of the acoustic sources. However, the noise generation mechanisms associated with turbomachinery are compl ...

    SBIRPhase I2004National Aeronautics and Space Administration

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