All Stories

  1. Wind and Turbulence Distributed Sensing for Advanced Air Mobility

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Thomas Lombaerts, Dr Kapil S Sheth

  2. Design and Testing of Gust Load Alleviation Control Laws for the IAWTM Wind Tunnel Test

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr. Thomas G Ivanco

  3. Design and Evaluation of Active Flutter Suppression Control Laws for the IAWTM Wind Tunnel Test

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Thomas G Ivanco, Dr Nhan Nguyen, Ryan Caverly

  4. Comparison of Methods for Efficient Static Wind Tunnel Testing Using Multiple Control Surfaces

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  5. Aeroservoelastic Flight Dynamic Modeling of Multi-Rotor eVTOL Aircraft

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  6. Experimental Verification of High-Fidelity Static Aeroelastic Load Predictions

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  7. High-Fidelity Flutter Prediction of Aspect Ratio 13.5 Flexible Wing Wind Tunnel Model

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  8. Nonlinear Time-Domain System Identification of Aircraft Stability and Control Derivatives

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  9. Interactions of Time-Scale Separated Hybrid Adaptive Systems

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  10. Analytical Flight Dynamic Model Development for eVTOL Aircraft

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  11. Nonlinear System Identification of Aircraft Stability Derivatives in Numerical Forced Oscillation Experiment

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  12. Distributed Hamiltonian Adaptive Disturbance Rejection Control With Actuator Dynamics

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  13. Modelling Dynamics of Highly Flexible Aircraft Using a Geometrically Nonlinear Structural Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  14. Study of Trailing Edge Mini-plain Flap Interactions on a Wind Tunnel Scale Aspect Ratio 13.5 Common Research Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  15. Reduced-Order Modelling for the Dynamics of Flexible Solar Sails

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  16. Wake Disturbance-Based Separation Evaluation for Urban Air Mobility Aircraft

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  17. Computationally Efficient Frequency Domain Method for Dynamic Control Derivative Estimation With Application to Transonic Truss-Braced Wing

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  18. Transonic Buffet Simulation of Mach 0.8 Transonic Truss-Braced Wing Aeroelastic Model

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  19. Multi-Objective Optimal Control of High Aspect Ratio Wing Wind Tunnel Model

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  20. Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  21. Aeroelastic Simulation of Wind Tunnel Scale Aspect Ratio 13.5 Common Research Model with Trailing Edge Mini-Flaps

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  22. Nonlinear Distributed Hamiltonian Control of Very Flexible Aircraft with Adaptive Gust Rejection

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  23. Nonlinear Dynamic Control Derivative Analysis for Aircraft Application to Transonic Truss-Braced Wing

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  24. Steady and Unsteady Simulations of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  25. Aeroelastic Trim Drag Optimization of Mach 0.8 Transonic Truss-Braced Wing Aircraft with Variable Camber Continuous Trailing Edge Flap

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  26. CFD-Based Frequency Domain Method for Dynamic Stability Derivative Estimation with Application to Transonic Truss-Braced Wing

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  27. Aeroservoelastic Flight Dynamic Modeling of UAM Conceptual Vehicles

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  28. Integrated Vehicle-Propulsion-Control Design Architecture for Distributed Electric Propulsion-Enabled Aircraft

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Sricharan Ayyalasomayajula, Dr Nhan Nguyen, Racheal Erhard

  29. Transonic Correction to Theodorsen's Theory for Oscillating Airfoil in Pitch and Plunge Toward Flutter

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  30. Hamiltonian Adaptive and Optimal Control of Lagrangian Infinite-Dimensional Systems with Gust Load Alleviation Application

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  31. A Physics-Based Spatial Wake Interactional Model of Fixed-Wing Aircraft and Rotorcraft for Urban Air Mobility

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  32. Multi-point Jig Twist Optimization of Mach 0.745 Transonic Truss-Braced Wing Aircraft and High-Fidelity CFD Validation

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Jason Fugate

  33. Aerodynamic Optimization of Mach 0.745 Transonic Truss-BracedWing Aircraft with Variable-Camber Continuous Trailing-Edge Flap

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  34. Real-Time Drag Optimization of Aspect Ratio 13.5 Common Research Model with Distributed Flap System

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  35. Aerodynamic analysis of a Flapping Transitional Configuration

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Luciano Demasi, Dr Nhan Nguyen

  36. Extending A Correction Method for Unsteady Transonic Aerodynamics to Variable Camber Continuous Trailing Edge Flap

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul

  37. Real-Time Adaptive Drag Minimization Wind Tunnel Investigation of a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  38. Aero-Structural Modeling of the Truss-Braced Wing Aircraft Using Potential Method with Correction Methods for Transonic Viscous Flow and Wing-Strut Interference Aerodynamics

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Jason Fugate, Dr Nhan Nguyen

  39. Computation of Flow Induced by Gust Generator in a Wind-Tunnel

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  40. Investigation of Truss-Braced Wing Aircraft Transonic Wing-Strut Interference Effects Using FUN3D

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Jason Fugate, Dr Nhan Nguyen

  41. RANS simulations of a pitching and plunging VCCTEF airfoil toward a transonic flutter model

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul, Dr Nhan Nguyen

  42. Optimal Control Design with Adaptive Nominal Loop

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  43. Investigation of Anti-Phase Asymmetric Quiet Rotor Technology

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  44. Multi-objective Optimal Control of the 6-DoF Aeroservoelastic Common Research Model with Aspect Ratio 13.5 Wing

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  45. Flutter Analysis of the Transonic Truss-Braced Wing Aircraft Using Transonic Correction

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul, Jason Fugate

  46. Time-Varying Weights in Multi-Objective Optimal Control for Flexible Wing Aircraft

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  47. Optimization of Variable-Camber Continuous Trailing-Edge Flap Configuration for Drag Reduction

    Article • Journal of Aircraft, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  48. Distributed Propulsion Aircraft with Aeroelastic Wing Shaping Control for Improved Aerodynamic Efficiency

    Article • Journal of Aircraft, May 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  49. Development of an Integrated Nonlinear Aeroservoelastic Flight Dynamic Model of the NASA Generic Transport Model

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  50. Large Deflection Aeroelasticity and Aeroelastic Lifting Line Theory for Examination of Aerodynamic Effects and Nonlinear Limit Cycle Oscillations

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  51. Output Feedback Adaptive Control of Non-Minimum Phase Systems Using Optimal Control Modification

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Ehsan Arabi

  52. Multi-Objective Adaptive Control for Load Alleviation and Drag Minimization of Flexible Aircraft

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  53. Stability limit of human-in-the-loop model reference adaptive control architectures

    Article • International Journal of Control, July 2017, Taylor & Francis

    Professor Yildiray Yildiz, Dr Nhan Nguyen

  54. Transonic and Viscous Potential Flow Method Applied to Flexible Wing Transport Aircraft

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Gustavo Eidji C Fujiwara

  55. Aero-Structural Optimization of Variable Camber Continuous Trailing Edge Flap Configurations Using Transonic and Viscous Potential Flow Method

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  56. Nonlinear Large Deflection Theory with Modified Aeroelastic Lifting Line Aerodynamics for a High Aspect Ratio Flexible Wing

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  57. Aeroestructural Design Optimization of a Subsonic Wing with Continuous Morphing Trailing Edge

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  58. A set-theoretic model reference adaptive control architecture for disturbance rejection and uncertainty suppression with strict performance guarantees

    Article • International Journal of Control, April 2017, Taylor & Francis

    Dr Nhan Nguyen, Ehsan Arabi

  59. Adaptive Disturbance Torque Estimation for Orbiting Spacecraft Using Recursive Least-Squares Methods

    Article • Journal of Aerospace Information Systems, February 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  60. LPV Model Development for a Flexible Wing Aircraft

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Sean Swei, Dr Nhan Nguyen, Professor Guoming George Zhu

  61. Development of an Integrated Nonlinear Aeroservoelastic Flight Dynamic Model of the Truss-Braced Wing Aircraft

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  62. Optimal Decentralized Controller with Output Feedback Design for an Elastically Shaped Aircraft Concept

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  63. Performance Optimizing Multi-Objective Adaptive Control with Time-Varying Reference Model Modification

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Ehsan Arabi

  64. Model Reference Neuroadaptive Control Revisited: How to Keep the System Trajectories on a Given Compact Set

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Ehsan Arabi

  65. Decentralized Optimal Adaptive Control Architectures for the VCCTEF Aircraft

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Professor james steck, Animesh Chakravarthy

  66. Multi-Objective Flight Control for Drag Minimization and Load Alleviation of High-Aspect Ratio Flexible Wing Aircraft

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  67. A Flutter Suppression and Drag Optimization Approach for Flexible Aircraft

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  68. Stability Analysis of Human-Adaptive Controller Interactions

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Yildiray Yildiz, Dr Nhan Nguyen

  69. Normalized Optimal Control Modification and Flight Experiments on NASA F/A-18 Aircraft

    Article • Journal of Guidance Control and Dynamics, July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  70. Static Aeroelastic Model Assessment in the Transonic Regime

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  71. Lift Optimization Study of a Multi-Element Three-Segment Variable Camber Airfoil

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul, Dr Nhan Nguyen

  72. An Integral Boundary Layer Direct Method Applied to 2D Transonic Small-Disturbance Equations

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  73. Real-Time Adaptive Least-Squares Drag Minimization for Performance Adaptive Aeroelastic Wing

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  74. Aerodynamic Modeling of Transonic Aircraft Using Vortex Lattice Coupled with Transonic Small Disturbance for Conceptual Design

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  75. Wing Shaping Concept for Distributed Propulsion Aircraft to Improve Aerodynamic Efficiency

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  76. Demonstration Platform for Trajectory Planning of an Autonomous Nonholonomic Skid-Steer System for Investigating Spatial Phenomena

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  77. Adaptive Estimation of Disturbance Torque for Orbiting Spacecraft Using Recursive Least Squares Method

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  78. Adaptive Modal Identification for Flutter Suppression Control

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  79. Fuzzy Model-Based Optimal Variance Control of Flexible Aircraft with Actuator Amplitude and Rate Constraints

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  80. Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  81. Wind Tunnel Investigation of a Flexible Wing High-Lift Configuration with a Variable Camber Continuous Trailing Edge Flap Design

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  82. Use of a Viscous Flow Simulation Code for Static Aeroelastic Analysis of a Wing at High-Lift Conditions

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  83. Adaptive Aeroelastic Wing Shape Optimization for High-Lift Configurations

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Gustavo Eidji C Fujiwara

  84. A 3-D Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul

  85. Unsteady Aeroservoelastic Modeling of Flexible Wing Generic Transport Aircraft with Variable Camber Continuous Trailing Edge Flap

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  86. Optimization for Load Alleviation of Truss-Braced Wing Aircraft With Variable Camber Continuous Trailing Edge Flap

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  87. Adaptive Linear Quadratic Gaussian Optimal Control Modification for Flutter Suppression of Adaptive Wing

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  88. Bayesian Modeling for Decentralized UAV Control and Task Allocation

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  89. A Design, Analysis and Verification Framework for Adaptive Flight Control

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  90. Aeroelastic Analysis of Wind Tunnel Test Data of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap (VCCTEF)

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  91. Static Aeroelastic Modeling of a Sub-Scale Wind Tunnel Model with Novel Flap Concept

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  92. Multidisciplinary Drag Optimization of Reduced Stiffness Flexible Wing Aircraft With Variable Camber Continuous Trailing Edge Flap

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  93. Aerodynamic Load Analysis of a Variable Camber Continuous Trailing Edge Flap System on a Flexible Wing Aircraft

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  94. Aeroelasticity of Axially Loaded Aerodynamic Structures for Truss-Braced Wing Aircraft

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  95. Comparison of Unsteady Aerodynamics Approximations for Time-Domain Representation of Frequency-Independent Aeroelastic State-Space Models

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  96. A Multi-Objective Flight Control Approach for Performance Adaptive Aeroelastic Wing

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  97. LMI-based Multiobjective Optimization and Control of Flexible Aircraft Using VCCTEF

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  98. Bi-objective optimal control modification adaptive control for systems with input uncertainty

    Article • IEEE/CAA Journal of Automatica Sinica, October 2014, Chinese Association of Automation

    Dr Nhan Nguyen

  99. Reinforcement learning based controller synthesis for flexible aircraft wings

    Article • IEEE/CAA Journal of Automatica Sinica, October 2014, Chinese Association of Automation

    Dr Nhan Nguyen

  100. Wing shaping concepts using distributed propulsion

    Article • Aircraft Engineering, September 2014, Emerald

    Dr Nhan Nguyen

  101. Experimental Investigation of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap Design

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  102. Aeroelastic Modeling and Drag Optimization of Flexible Wing Aircraft with Variable Camber Continuous Trailing Edge Flap

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  103. Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul

  104. Aerodynamic Analysis of the Truss-Braced Wing Aircraft Using Vortex-Lattice Superposition Approach

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  105. Multi-Objective Optimal Control Modification Adaptive Control Method for Systems with Input and Unmatched Uncertainties

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  106. Static Aeroelastic and Longitudinal Trim Model of Flexible Wing Aircraft Using Finite-Element Vortex-Lattice Coupled Solution

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  107. Static Aeroelastic Scaling and Analysis of a Sub-Scale Flexible Wing Wind Tunnel Model

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  108. Flutter Analysis of Mission-Adaptive Wing with Variable Camber Continuous Trailing Edge Flap

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  109. Flight Dynamic Modeling and Stability Analysis of Flexible Wing Generic Transport Aircraft

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  110. Aeroelastic Wing Shaping Control Subject to Actuation Constraints

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Sean Swei

  111. Optimal and Decentralized Controller Designs for an Elastically Shaped Aircraft

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Animesh Chakravarthy

  112. Lyapunov Stability Analysis of an Aeroleastic Torsion Model

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  113. A Preliminary Study for Optimal Longitudinal-Mode Flight Control through Distributed Aeroelastic Shaping

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen

  114. Demonstration of the Optimal Control Modification for 6-DOF Control of a General Aviation Aircraft

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Professor james steck