Advanced Dynamics, Inc.

1500 Bull Lea Road, Suite 203
Lexington, KY 40511
http://www.advanceddynamics-usa.com
15 Employees

SBIR Award Summary

Total Number of Awards 19
Total Value of Awards $3.43MM
First Award Date 01/01/07
Most Recent Award Date 02/15/12

Key Personnel

Last Name Name Awards Contact
Hu Dr. Patrick Hu 19 Message
Zabaras Nicholas Zabaras 1 Message
Ni Kan Ni 1 Message

19 Awards Won

Phase 1 STTR

Institution: Arizona State University

Agency: Air Force
Topic: AF11-BT22
Budget: 02/15/12 - 11/14/12
PI: Kan Ni

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 protocol assumes that only one mode is present and only provides upper and lower bound estimates of the blade peak stress when multiple modes are imp...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 10-1-A2.04
Budget: 01/01/11 - 12/31/11

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 shedding, shock-turbulence interaction, separation, etc. dominate at transonic and supersonic Mach numbers and hence the need to address these phen...

Phase 2 SBIR

Agency: National Aeronautics and Space Administration
Topic: 09-2-A2.04
Budget: 01/01/11 - 12/31/11

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 quantification for data-driven risk analysis and certification. A number of novel reduced-order in time methods will be implemented into the code all...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 10-1-A2.04
Budget: 01/01/11 - 12/31/11

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 surfaces with varying amounts of freeplay and their aeroelastic response. These methods will be validated with wind tunnel and flight test data. In P...

Phase 1 STTR

Institution: University of Missouri Rolla

Agency: Navy
Topic: N10A-T010
Budget: 07/30/10 - 02/28/11

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 loading by foreign objects. In particular, the physics-based model will be applied to describe the multiscale foreign object damage (FOD) phenomena of C...

Phase 1 STTR

Institution: University of Oklahoma

Agency: Navy
Topic: N10A-T003
Budget: 07/30/10 - 02/28/11

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 limit cycle oscillation characteristics of two-dimensional and three-dimensional wings in subsonic and transonic flow. Highly efficient and accurat...

Phase 1 STTR

Institution: Cornell University

Agency: Navy
Topic: N10A-T028
Budget: 06/28/10 - 04/30/11

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 supperalloys which have high creep and oxidation resistance at high temperatures are widely used as the material of turbine disks. The elevated-temperat...

Phase 1 STTR

Institution: University of California, Irvine

Agency: Navy
Topic: N10A-T041
Budget: 06/28/10 - 04/30/11

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, marine ships are subjected to a complex and severe loading, and the typical failure mode of aluminum under extreme dynamics loading such as wave sl...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 10-1-A2
Budget: 01/01/10 - 12/31/10

Research is proposed for the development and implementation of state of the art, reduced order models for problems in

Phase 2 SBIR

Agency: Army
Topic: A08-022
Budget: 10/20/09 - 10/19/11

This SBIR aims at developing a high-fidelity, yet efficient and easy-to-use, composite rotor blade and wing section design environment to facilitate rapid and confident aeromechanics assessment during conceptual design stages. A well-known technical barrier for composite rotor blade and wing section design is the lack of a user friendly, efficie...

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