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Wei Zhao

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Oklahoma State University

United States

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NASA NRA: Wing Structural Design for Enhanced performance

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Subsonic Fixed Wing Program

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Articles (17)

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2026

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Collaborators (4)

Jian Yang

University of Nottingham Ningbo China (UNNC)

CHINA

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Rakesh Kapania

Wendy and Norris Mitchell Professor

Virginia Tech

UNITED STATES

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Caitlyn Clarkson

R&D Staff Scientist

Oak Ridge National Laboratory

UNITED STATES

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Shuvodeep De

Texas State University

UNITED STATES

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Wei Zhao

Research Interests

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Recent Grants

Articles (17)

Convolutional Neural Network and Image Processing-Based Approach for Homogenization of Lattice Structures

Multi-Scale Microstructure-Informed Modeling of Residual Stresses and Distortions in Additive Friction Stir Deposition

Robotic Kinematic Modeling and Deformation of Composite Laminates via Automated Fiber Placement Manufacturing

Towpreg-wise Modeling for Composite Laminates Manufactured via Automated Fiber Placement

Wrinkle Deformation of Curved Prepreg Slit-Tapes Tow-Steered Laminates During Automated Fiber Placement

Additive Manufacturing with Cellulose‐Based Composites: Materials, Modeling, and Applications

Theoretical and experimental analyses of beam-like inflatables

Analytical and neural network-based approaches for mechanical postbuckling analysis of simply-supported functionally graded graphene origami-enabled auxetic metamaterial plates

Buckling of variable angle tow steered laminates considering gap/overlap defects identified using innovative image processing

Jacobi–Ritz Method for Buckling of Unitized Curvilinearly Stiffened Functionally Graded Plates

Tightly Coupled Geometrically Nonlinear Structural and Aeroelastic Analysis of Flexible Wing Plate Model

Vibration Analysis of Tow-Steered Laminates Considering Overlaps/Gaps Identified from Image Processing

Two-Level Weight Optimization of Composite Laminates Using Integer Programming

Buckling Analysis and Optimization of Stiffened Variable Angle Tow Laminates with a Cutout Considering Manufacturing Constraints

Skin-stringer assembly using radial basis functions for curvilinearly stiffened panels

Actuator energy and drag minimization of a blended-wing-body with variable-camber continuous trailing-edge flaps

Controllability gramian as control design objective in aircraft structural design optimization

Collaborators (4)

Jian Yang

Rakesh Kapania

Caitlyn Clarkson

Shuvodeep De

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