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

56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ◽

10.2514/6.2015-1408 ◽

2015 ◽

Author(s):

Sonia Lebofsky ◽

Eric Ting ◽

Nhan T. Nguyen

Keyword(s):

Trailing Edge ◽

Flexible Wing ◽

Trailing Edge Flap

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

32nd AIAA Applied Aerodynamics Conference ◽

10.2514/6.2014-2443 ◽

2014 ◽

Author(s):

Sonia Lebofsky ◽

Eric Ting ◽

Nhan T. Nguyen ◽

Khanh V. Trinh

Keyword(s):

Trailing Edge ◽

Flexible Wing ◽

Trailing Edge Flap

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

56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ◽

10.2514/6.2015-1405 ◽

2015 ◽

Author(s):

Nhan T. Nguyen ◽

Eric Ting ◽

Sonia Lebofsky

Keyword(s):

Wind Tunnel ◽

Test Data ◽

Wind Tunnel Test ◽

Trailing Edge ◽

Flexible Wing ◽

Aeroelastic Analysis ◽

Trailing Edge Flap

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Coupled Vortex-Lattice Flight Dynamic Model with Aeroelastic Finite-Element Model of Flexible Wing Transport Aircraft with Variable Camber Continuous Trailing Edge Flap for Drag Reduction

10.2514/6.2013-4746 ◽

2013 ◽

Author(s):

Nhan T. Nguyen ◽

Eric B. Ting ◽

Daniel Nguyen ◽

Tung Dao ◽

Khanh Trinh

Keyword(s):

Finite Element ◽

Finite Element Model ◽

Drag Reduction ◽

Dynamic Model ◽

Vortex Lattice ◽

Element Model ◽

Trailing Edge ◽

Transport Aircraft ◽

Flexible Wing ◽

Trailing Edge Flap

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Progress on Gust Load Alleviation Wind Tunnel Experiment and Aeroservoelastic Model Validation for a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System

AIAA Scitech 2020 Forum ◽

10.2514/6.2020-0214 ◽

2020 ◽

Author(s):

Nhan T. Nguyen ◽

Nick B. Cramer ◽

Kelley E. Hashemi ◽

Michael C. Drew ◽

Juntao Xiong ◽

...

Keyword(s):

Wind Tunnel ◽

Model Validation ◽

Wind Tunnel Experiment ◽

Trailing Edge ◽

Flexible Wing ◽

Trailing Edge Flap ◽

Gust Load Alleviation

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

AIAA Aviation 2019 Forum ◽

10.2514/6.2019-3156 ◽

2019 ◽

Author(s):

Nhan T. Nguyen ◽

Nick B. Cramer ◽

Kelley E. Hashemi ◽

Eric Ting ◽

Michael Drew ◽

...

Keyword(s):

Wind Tunnel ◽

Real Time ◽

Trailing Edge ◽

Flexible Wing ◽

Drag Minimization ◽

Trailing Edge Flap

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

56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ◽

10.2514/6.2015-1839 ◽

2015 ◽

Author(s):

Eric Ting ◽

Tung Dao ◽

Nhan T. Nguyen

Keyword(s):

Aerodynamic Load ◽

Trailing Edge ◽

Flexible Wing ◽

Load Analysis ◽

Trailing Edge Flap

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

32nd AIAA Applied Aerodynamics Conference ◽

10.2514/6.2014-2441 ◽

2014 ◽

Author(s):

Nhan T. Nguyen ◽

Eli Livne ◽

Nathan Precup ◽

James M. Urnes ◽

Chester Nelson ◽

...

Keyword(s):

Experimental Investigation ◽

Trailing Edge ◽

Flexible Wing ◽

Flap Design ◽

Trailing Edge Flap

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

33rd AIAA Applied Aerodynamics Conference ◽

10.2514/6.2015-2417 ◽

2015 ◽

Author(s):

Nhan T. Nguyen ◽

Nathan Precup ◽

Eli Livne ◽

James M. Urnes ◽

Eric Dickey ◽

...

Keyword(s):

Wind Tunnel ◽

Trailing Edge ◽

High Lift ◽

Flexible Wing ◽

Flap Design ◽

Trailing Edge Flap

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

33rd AIAA Applied Aerodynamics Conference ◽

10.2514/6.2015-2722 ◽

2015 ◽

Author(s):

Ezra A. Tal ◽

Nhan T. Nguyen

Keyword(s):

Trailing Edge ◽

Transport Aircraft ◽

Flexible Wing ◽

Trailing Edge Flap

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Effects of torsion frequencies on rotor performance and structural loads with trailing edge flap

Smart Materials and Structures ◽

10.1088/0964-1726/21/8/085026 ◽

2012 ◽

Vol 21 (8) ◽

pp. 085026 ◽

Author(s):

Rohit Jain ◽

Hyeonsoo Yeo

Keyword(s):

Trailing Edge ◽

Trailing Edge Flap

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