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A Variable-fidelity Simulation Tool for Dynamic Non-linear Fluid/Structure Interaction Problems
Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9550-06-C-0116
Agency Tracking Number: F064-016-0281
Amount:
$100,000.00
Phase:
Phase I
Program:
STTR
Solicitation Topic Code:
AF06-T016
Solicitation Number:
N/A
Timeline
Solicitation Year:
2006
Award Year:
2006
Award Start Date (Proposal Award Date):
2006-09-30
Award End Date (Contract End Date):
2007-06-30
Small Business Information
11785 Beltsville Drive, 9th Floor
Beltsville, MD
20705
United States
DUNS:
061997029
HUBZone Owned:
No
Woman Owned:
No
Socially and Economically Disadvantaged:
No
Principal Investigator
Name: Peter Chen
Title: Principal Investigator
Phone: (240) 790-0608
Email: chenp@technosci.com
Title: Principal Investigator
Phone: (240) 790-0608
Email: chenp@technosci.com
Business Contact
Name: Amy Hizoune
Title: VP, Finance
Phone: (240) 790-0609
Email: aph@technosci.com
Title: VP, Finance
Phone: (240) 790-0609
Email: aph@technosci.com
Research Institution
N/A
Abstract
Techno-Sciences, Inc. (TSi), in collaboration with the Smart Structures Laboratory of the Alfred Gessow Rotorcraft Center at the University of Maryland (UMD), propose to develop a high-fidelity fluid-structure interaction model that is uniquely suited to morphing wing aeroelastic and response prediction. We propose to produce a flapping wing fluid-structure interaction (FWFSI) analysis method to develop an aeroelastic stability augmentation (AESA) system and response prediction for morphing aircraft. A framework will be constructed by link all necessary components in the FWFSI model and the analytical results will be validated using an existing database of experimental results.
* Information listed above is at the time of submission. *
