Advanced Dynamics, Inc.

Basic Information

KY
Lexington, KY, 40511-1628

http://www.advanceddynamics-usa.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 790637867
Hubzone Owned: N
Socially and Economically Disadvantaged: Y
Woman Owned: N
Number of Employees: 15


  1. An Innovative Software Tool for Blades Stress Estimation during Multiple Simultaneous Vibratory Mode

    Amount: $99,996.00

    ABSTRACT: ADI and ASU propose to develop a novel methodology for blade peak stress prediction from limited strain gage/tip-timing measurements when multiple vibratory modes are present. The current p ...

    STTR Phase I 2012 Air ForceDepartment of DefenseDepartment of Defense
  2. State-of-the-art, Multi-Fidelity Modeling and Simulation (M&S) Tool for Nonlinear Aeroelasticity

    Amount: $600,000.00

    Research is proposed for the development of a state-of-the-art computational aeroelastic tool. This tool will include various levels of fidelity and the ability to perform computational uncertainty qu ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  3. High Fidelity Computational and Wind Tunnel Models in Support of Certification Airworthiness of Control Surfaces with Freeplay and Other Nonlinear Features

    Amount: $98,373.00

    The proposed work will establish high fidelity computational methods and wind tunnel test model in support of new freeplay criteria for the design, construction and controlled actuation of control su ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  4. Towards Better Modeling and Simulation of Nonlinear Aeroelasticity On and Beyond Transonic Regimes

    Amount: $99,577.00

    The need to accurately predict aeroelastic phenomenon for a wide range of Mach numbers is a critical step in the design process of any aerospace vehicle. Complex aerodynamic phenomenon such as vortex ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  5. Novel Reduced Order in Time Models for Problems in Nonlinear Aeroelasticity

    Amount: $99,966.00

    Research is proposed for the development and implementation of state of the art, reduced order models for problems in nonlinear aeroelasticity. Highly efficient and accurate aeroelastic simulation too ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  6. Meshfree-Based Fracture Evaluation and Design Tool for Welded Aluminum Ship Structures

    Amount: $70,000.00

    The aluminum alloys have low density, relatively high strength, and high strength-to-weight ratio, which brings some major advantages in marine structure design, fabrication, and operations. However, ...

    STTR Phase I 2010 NavyDepartment of DefenseDepartment of Defense
  7. Deterministic and Statistical Characterization of the Impact of Control Surface Freeplay on Flutter and Limit-Cycle Oscillation (LCO) using Efficient

    Amount: $70,000.00

    Research is proposed for the development and implementation of state of the art computational and experimental tools for the investigation of the impact of control surface freeplay on the flutter and ...

    STTR Phase I 2010 NavyDepartment of DefenseDepartment of Defense
  8. Multiscale Modeling and Analysis of Foreign Object Damage in Ceramic Matrix Composites with the Material Point Method

    Amount: $70,000.00

    This Small Business Technology Transfer Phase I project is aiming at developing and implementing a multiscale composite model to predict the ceramic matrix composite (CMC) response to the impact loadi ...

    STTR Phase I 2010 NavyDepartment of DefenseDepartment of Defense
  9. STOCHASTIC MUTISCALE/MULTISTAGE MODELING OF ENGINE DISKS

    Amount: $70,000.00

    Turbine disks are amongst the most critical components in aero- and naval-vessel engines. They operate in a high pressure and temperature environment requiring demanding properties. Nickel-based suppe ...

    STTR Phase I 2010 NavyDepartment of DefenseDepartment of Defense
  10. Physics-Based Identification, Modeling and Risk Management for Aeroelastic Flutter and Limit-Cycle Oscillations (LCO)

    Amount: $99,938.00

    The proposed research program will develop a physics-based identification, modeling and risk management infrastructure for aeroelastic transonic flutter and limit-cycle oscillations (LCO). This capabi ...

    SBIR Phase I 2009 National Aeronautics and Space Administration

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