Title page for ETD etd-03172010-020348


Type of Document Master's Thesis
Author Luton, J. Alan
URN etd-03172010-020348
Title Numerical simulations of subsonic aeroelastic behavior and flutter suppression by active control
Degree Master of Science
Department Engineering Mechanics
Advisory Committee
Advisor Name Title
Mook, Dean T. Committee Chair
Hendricks, Scott L. Committee Member
Nayfeh, Ali H. Committee Member
Keywords
  • Flutter (Aerodynamics)
Date of Defense 1991-12-15
Availability restricted
Abstract

A method for predicting the unsteady, subsonic, aeroservoelastic response of a wing has been developed. The air, wing, and control surface are considered to be a single dynamical system. All equations are solved simultaneously in the time domain by a predictor-corrector method. The scheme allows nonlinear aerodynamic and structural models to be used and subcritical, critical, and supercritical aeroelastic behavior may be modeled without restrictions to small disturbances or periodic motions. A vortex-lattice method is used to model the aerodynamics. This method accounts for nonlinear effects associated with high angles of attack, unsteady behavior, and deformations of the wing. The vortex-lattice method is valid as long as separation or vortex bursting does not occur. Two structural models have been employed: a linear model and a nonlinear model which accounts for large curvature. Both models consider the flexural-torsional motion of an inextensional wing.

Files
  Filename       Size       Approximate Download Time (Hours:Minutes:Seconds) 
 
 28.8 Modem   56K Modem   ISDN (64 Kb)   ISDN (128 Kb)   Higher-speed Access 
[VT] LD5655.V855_1991.L876.pdf 3.14 Mb 00:14:32 00:07:28 00:06:32 00:03:16 00:00:16
[BTD] next to an author's name indicates that all files or directories associated with their ETD are accessible from the Virginia Tech campus network only.

Browse All Available ETDs by ( Author | Department )

dla home
etds imagebase journals news ereserve special collections
virgnia tech home contact dla university libraries

If you have questions or technical problems, please Contact DLA.