# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# educationAndTraining[].organization.label
Virginia Tech - (Blacksburg, Virginia, United States)

# publications[].label
Control of a nonlinear wing section using leading- and trailing-edge surfaces

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Studies of Store-Induced Limit Cycle Oscillations Using a Model with Full System Nonlinearities

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Store-induced limit cycle oscillations and internal resonances in aeroelastic systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Suppressing aeroelastic instability using broadband passive targeted energy transfers, part 2: Experiments

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A Finite element-Multibody dynamics co-simulation methodology applied to FAST

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Computational and experimental fluid-structure interaction assessment of a high-lift wing with a slat-cove filler for noise reduction

# publications[].label
NOISE REDUCTION IN A HIGH LIFT WING USING SMAS: COMPUTATIONAL FLUID-STRUCTURAL ANALYSIS

# publications[].label
The investigation of balloon materials exposed to the low earth orbit environment

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A Finite element-Multibody dynamics co-simulation methodology applied to FAST

# publications[].publisher
American Institute of Aeronautics and Astronautics

# publications[].label
Experimental validation of a shape-memory alloy slat-cove filler: Structural response and computational model development

# publications[].label
Aeroelastic response of a rigid wing supported by nonlinear springs

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
The nonlinear biaxial characterization of balloon film

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Aeroelastic behavior of composite plates subject to damage growth

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
The numerical simulation of subsonic flutter

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Suppression of aeroelastic instability with a nonlinear energy sink: Experimental results

# publications[].label
A Comprehensive Approach to Simulate Nonlinear Aeroelastic Response

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear responses of a cantilever wing with an external store

# publications[].label
Identification and control of limit cycle oscillations in aeroelastic systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A Parallel Multigrid Algorithm for Aeroelasticity Simulations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Unsteady Aerodynamic Model Based on the Leading-Edge Stagnation Point

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Morphing Aircaft Dynamical Model: Longitudinal Shape Changes

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Stability and control of a structurally nonlinear aeroelastic system

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Aeroelastic Studies of a Cantilever Wing with Structural and Aerodynamic Nonlinearities

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear Responses of a Cantilever Wing with an External Store

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity

# publications[].label
Gust Load Alleviation of an Aeroelastic System Using Nonlinear Control

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A laser scanning graphic system for multimedia podium presentations

# publications[].publisher
SPIE, the international society for optics and photonics

# publications[].label
Control of aeroelastic response via synthetic jet actuators

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Dynamic response and game theoretic control of evolving structural systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Physics-Based Aeroelastic Analysis for Future Air Vehicle Concepts Using a Fully Nonlinear Methodology

# publications[].label
NUMERICAL-MODEL OF UNSTEADY SUBSONIC AEROELASTIC BEHAVIOR

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Parallel Multigrid Algorithm for Aeroelasticity Simulations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experiments in free and forced aeroelastic response

# publications[].label
PHYSICAL CHARACTERIZATION OF THIN-FILM POLYMERS EXPOSED TO THE LOW EARTH ORBIT ENVIRONMENT

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
THE EFFECT OF DAMAGE GROWTH ON THE AEROELASTIC RESPONSE OF COMPOSITE STRUCTURES

# publications[].label
Experimentation and Computational Assessment of an SMA-Based Slat-Cove Filler For Noise Reduction in a High Lift Wing

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Aeroelastic Analysis for Future Air Vehicle Concepts Using a Fully Nonlinear Methodology

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A new method to predict unsteady aeroelastic behavior

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses

# publications[].label
Viscoelastic characterization of thin-film materials using a dynamic mechanical approach

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Application of the unsteady vortex-lattice method to the nonlinear two-degree-of-freedom aeroelastic equations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experiments of Vortex-Induced Vibration of a Flat Plate Exposed to a Normal Cross Flow

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Suppression of control reversal using leading- and trailing-edge control surfaces

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear Control Methods for High-Energy Limit-Cycle Oscillations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Studies of store-induced limit-cycle oscillations using a model with full system nonlinearities

# publications[].label
Nonlinear Control Methods for High Energy Limit Cycle Oscillations

# publications[].label
Computational and experimental investigation of limit cycle oscillations in nonlinear aeroelastic systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear aeroelastic response of an airfoil

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear control of a prototypical wing section with torsional nonlinearity

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Analyses and experiments of suppression of control reversal using a wing section with multiple control surfaces

# publications[].label
Flow separation control via synthetic jet actuation

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An approach for prescribed experiments for aerodynamic-structural dynamic interaction

# publications[].label
Control of a Wing Section With Structural Nonlinearities Using Leading and Trailing Edge Control Surfaces

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Analysis and simulation of polymers exposed to low earth orbit (LEO)environments

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Higher-Order Spectral Analysis of a Nonlinear Pitch and Plunge Apparatus

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Transonic Aeroelastic Instability Suppression for a Swept Wing by Targeted Energy Transfer

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An Unsteady Aerodynamic Model based on the Leading-Edge Stagnation Point

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ANALYSIS OF VIBRATIONS OF THE NATIONAL TRANSONIC FACILITY MODEL SUPPORT SYSTEM USING A 3-D AEROELASTIC CODE

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Stability Enhancement of a Transonic Wing Using a Simple Passive Attachment

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Adaptive Feedback Linearization for the Control of a Typical Wing Section With Structural Nonlinearity

# publications[].label
A Load-Based Feedback Approach for Distributed Aeroservoelastic Control

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear Model Reference Adaptive Control for Limit Cycle Oscillations

# publications[].label
Nonlinear control theory for a class of structural nonlinearities in a prototypical wing section

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Identification and control of limit cycle oscillations in aeroelastic systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A Novel Method for Prediction of Nonlinear Aeroelastic Responses

# publications[].label
Applied active control for a nonlinear aeroelastic structure

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
The Effects of External Stores on Nonlinear Aeroelastic Responses

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Aerostructural and Aeroacoustic Experimental Testing of Shape Memory Alloy Slat Cove Filler

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Studies of store-induced limit-cycle oscillations using a model with full system nonlinearities

# publications[].label
Experiments in Aeroelastic Response and Control under Gust

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear control methodologies for hysteresis in PZT actuated on-blade elevons

# publications[].publisher
American Society of Civil Engineers (ASCE)

# publications[].label
Nonlinear aeroelastic response - Analyses and experiments

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Six Degree-of-Freedom Dynamical Model of a Morphing Aircraft

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
REDUCTION OF ACTUATION LOADS IN A SELF-DEPLOYING SMA-BASED SLAT-COVE FILLER FOR A TRANSPORT AIRCRAFT

# publications[].label
Multiresolution methods for reduced order models for dynamical systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experiments in Aeroelastic Response and Control under Gust

# publications[].publisher
American Institute of Aeronautics and Astronautics

# publications[].label
Investigations of aeroelastic response for a system with continuous structural nonlinearities

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Suppression of Limit Cycle Oscillations with a Nonlinear Energy Sink: Experimental Results

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
CHARACTERIZATION OF POLYMER-FILMS RETRIEVED FROM NASA LONG-DURATION EXPOSURE FACILITY

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An investigation of internal resonance in aeroelastic systems

# publications[].label
Nonlinear adaptive control of an aeroelastic system via geometric methods

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Structured model reference adaptive control for a wing section with structural nonlinearity

# publications[].label
Nonlinear analysis of store-induced limit cycle oscillations

# publications[].label
On the presence of internal resonances in aeroelastic systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Calculation of Numerical Boundary Measure for Wavelet-Galerkin Approximations in Aeroelasticity

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Wavelet Galerkin METHODES FOR GAME THEORETIC CONTROL OF DISTRIBUTED PARAMETER SYSTEMS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear Aeroelastic Response of the Flexible Wing in Trim

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experiments of vortex-induced vibration of a flat plate exposed to a normal cross flow

# publications[].label
Parallel Algorithm for Fully Nonlinear Aeroelastic Analysis

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems

# publications[].label
Modelling and Suboptimal Trajectory Generation for a Symmetric Flapping Wing Vehicle

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
CHARACTERIZATION OF NONLINEAR VISCOELASTIC BEHAVIOR USING A DYNAMIC-MECHANICAL APPROACH

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Multiwavelets and Particle Image Velocimetry methods

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses

# publications[].label
Constraint violation in concurrent range space methods for transient dynamic analysis

# publications[].label
Analyses and Experiments of Suppression of Control Reversal Using a Wing Section with Multiple Control Surfaces

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Aeroelastic Analysis of a Transonic Wing for Design of Local Nonlinear Attachments

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Robust Control of Distributed Parameter Systems with Structured Uncertainty

# publications[].label
A study of aeroelastic stability for the model support system of theNational Transonic Facility

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
AERODYNAMIC AND STRUCTURAL EVALUATION OF AN SMA SLAT-COVE FILLER USING COMPUTATIONAL AND EXPERIMENTAL TOOLS AT MODEL SCALE

# publications[].label
Control of a Nonlinear Wing Section using Fly-by-Feel Sensing

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Predictions of nonlinear viscoelastic behavior using a hybrid approach

# publications[].label
An approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses

# publications[].label
Experiments of Vortex-Induced Torsional Oscillation of a Flat Plate in Cross Flow

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Measurement and Modeling of Aeroelastic Response under Gust

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Multiresolution Methods for Reduced-Order Models for Dynamical Systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ON NONLINEAR VISCOELASTIC ANALYSIS OF THIN FILM MATERIALS USING A DYNAMIC MECHANICAL APPROACH

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A test and analysis protocol to rapidly characterize nonlinear viscoelastic properties of balloon materials

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Flutter Suppression of an Aeroelastic Wing Using Aerodynamic Observables, Leading-Edge, and Trailing-Edge Control Surfaces

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Static Nonlinear Aeroelastic Analysis of a Blended Wing Body

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# streetAddress
Texas A&M University; Aerospace Engineering; 3141 TAMU

# etdChairOf[].label
Jackson, Justin Patrick (2008-08). Modelling and control of a symmetric flapping wing vehicle: an optimal control approach. Master's Thesis.

# etdChairOf[].label
Johnson, Kristen Holmstrom (2010-08). Reduced-sensing Control Methods for Infinite-dimensional Systems. Master's Thesis.

# etdChairOf[].label
Nichkawde, Chetan (2003-05). Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation. Master's Thesis.

# etdChairOf[].label
Kutz, Douglas M (2014-05). An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models. Master's Thesis.

# etdChairOf[].label
Babbar, Yogesh (2015-05). Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads. Doctoral Dissertation.

# etdChairOf[].label
Lucas, Amy Marie (2009-08). Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control. Master's Thesis.

# etdChairOf[].label
Yang, Yi (2010-12). Experimental Investigations of Vortex Induced Vibration of A Flat Plate in Pitch Oscillation. Master's Thesis.

# etdChairOf[].label
Kim, Kiun (2004-09). Nonlinear aeroelastic analysis of aircraft wing-with-store configurations. Doctoral Dissertation.

# etdChairOf[].label
Scholten, William David (2016-12). Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction. Master's Thesis.

# etdChairOf[].label
Suryakumar, Vishvas Samuel (2013-05). A Finite Element-Multibody Dynamics Co-simulation Methodology Applied to FAST. Master's Thesis.