Nonlinear Reduced Order Modeling of Limit Cycle Oscillations of Aircraft Wiings

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F49620-01-C-0029
Agency Tracking Number: 99AFO221
Amount: $0.00
Phase: Phase I
Program: STTR
Awards Year: 2001
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
7430 E. Stetson Dr. Ste 205, Scottsdale, AZ, 85251
DUNS: 182103291
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Ping Chih Chen
 (480) 945-9988
Business Contact
 Danny Liu
Phone: (480) 945-9988
Research Institution
 Judith Dillon
 Department of Mechanical Engineering
Durham, NC, 27708
 (919) 684-2418
 Nonprofit college or university
The Zona technology/Duke University team process a challenging set of tasks to be accomplished in two years time that builds upon the very substantial progress already made in Phase I. Specifically, the 2D, Euler Euations CFD model (developed in Phase I)that uses a harmonic balance solution technique will be extended to include teh effects of viscosity (Navier-Stoke equations)and multiple structural modes. In parrallel teh 3D, Euler Equations CFD time linearized model (also developed in Phase I) whichalready includes multiple structural modes and uses a POD/ROM solution method will be extended to now include full dynamic nonlinear effects using harmonic balance solution; and then furtherextended to now include full dynamic nonlinear effecrs using aharmonic balance solution; and then further extended to include the effects of multi-bodies (e.g. wings plus tip missiles and stores).

* Information listed above is at the time of submission. *

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