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Deterministic and Statistical Characterization of the Impact of Control Surface…

Award Information

Agency:
Department of Defense
Branch:
Navy
Award ID:
95194
Program Year/Program:
2010 / STTR
Agency Tracking Number:
N10A-003-0328
Solicitation Year:
N/A
Solicitation Topic Code:
NAVY 10T003
Solicitation Number:
N/A
Small Business Information
Advanced Dynamics, Inc.
1500 Bull Lea Road, Suite 203 Lexington, KY 40511-
View profile »
Woman-Owned: No
Minority-Owned: Yes
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 2010
Title: Deterministic and Statistical Characterization of the Impact of Control Surface Freeplay on Flutter and Limit -Cycle Oscillation (LCO) using Efficient
Agency / Branch: DOD / NAVY
Contract: N68335-10-C-0411
Award Amount: $70,000.00
 

Abstract:

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 accurate aeroelastic simulation tools will be constructed based upon the following novel concepts 1) reduced order in time models based upon the mathematical formalism of optimal prediction theory 2) high-fidelity aeroelastic simulation based upon the coupling of a particle-method based CFD method to a nonlinear finite element structural dynamics solver and 3) reduced order in spatial models based upon proper orthogonal decomposition (POD) and Volterra theory. In addition, the proposed work will include the use of computational uncertainty quantification which will address, using a probabilistic approach, questions pertaining to the sensitivity of flutter and limit cycle oscillation with respect to possibly uncertain model input parameters such as the amount of freeplay and the freeplay stiffness. Legacy wind tunnel data along with new tests for the transonic regime will be used to validate and improve the computational models and to provide further insight into the complex phenomena of freeplay-induced flutter and limit cycle oscillations.

Principal Investigator:

Patrick Hu
President
8596990441
patrick.g.hu@advanceddynamics-usa.com

Business Contact:

Patrick Hu
President
8596990441
patrick.g.hu@advanceddynamics-usa.com
Small Business Information at Submission:

Advanced Dynamics, Inc.
1500 Bull Lea Road, Suite 203 Lexington, KY 40511

EIN/Tax ID: 510617963
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
Research Institution Information:
University of Oklahoma
865 Asp Ave.
Felgar Hall Room 212
Norman, OK 73019
Contact: Peter Attar
Contact Phone: 4053251749