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Prestressed Vibration of Stiffened Variable-Angle Tow Laminated Plates

AIAA journal, 2019-06, Vol.57 (6), p.2575-2593

2019

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Topology optimization with advanced CNN using mapped physics-based data

Structural and multidisciplinary optimization, 2023, Vol.66 (1), p.21, Article 21

2023

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Development of Deep Convolutional Neural Network for Structural Topology Optimization

AIAA journal, 2023-03, Vol.61 (3), p.1366-1379

2023

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Comparative Study of Skin–Stringer Connection Approaches for Stiffened Structures with Curvilinear Stiffeners

AIAA journal, 2023-10, Vol.61 (10), p.4632-4651

2023

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Isogeometric Thermal Buckling and Sensitivity Analysis of Periodically Supported Laminated Composite Beams

AIAA journal, 2022-05, Vol.60 (5), p.3215-3224

2022

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Bilevel Programming Weight Minimization of Composite Flying-Wing Aircraft with Curvilinear Spars and Ribs

AIAA journal, 2019-06, Vol.57 (6), p.2594-2608

2019

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Tire mode shape categorization using Zernike annular moment and machine learning classification

Scientific reports, 2024-04, Vol.14 (1), p.9482-9482, Article 9482

2024

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ALGA: Active Learning-Based Genetic Algorithm for Accelerating Structural Optimization

AIAA journal, 2021-01, Vol.59 (1), p.330-344

2021

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Thermal Buckling Analysis and Optimization of Curvilinearly Stiffened Plates with Variable Angle Tow Laminates

Journal of spacecraft and rockets, 2019-07, Vol.56 (4), p.1189-1204

2019

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Buckling and Prestressed Vibrations of Periodic Nonprismatic Beams Using Integral Equation Approach

AIAA journal, 2022-02, Vol.60 (2), p.925-937

2022

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Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization

AIAA journal, 2020-07, Vol.58 (7), p.3199-3220

2020

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Optimization of Hybrid Composite Laminates with Distinct Ply Thicknesses Using Integer Programming

AIAA journal, 2023-12, Vol.61 (12), p.5609-5619

2023

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Skin-Stringer Assembly Using Radial Basis Functions for Curvilinearly Stiffened Panels

AIAA journal, 2021-03, Vol.59 (3), p.1125-1133

2021

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Two-Level Weight Optimization of Composite Laminates Using Integer Programming

AIAA journal, 2022-11, Vol.60 (11), p.6436-6446

2022

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Vibration Analysis of Curvilinearly Stiffened Composite Panel Subjected to In-Plane Loads

AIAA journal, 2017-03, Vol.55 (3), p.981-997

2017

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A sensitivity-based nonlinear finite element model updating method for nonlinear engineering structures

Applied Mathematical Modelling, 2021-12, Vol.100, p.632-655

2021

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Global/Local Optimization of Aircraft Wing Using Parallel Processing

AIAA journal, 2016-11, Vol.54 (11), p.3338-3348

2016

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Vibration of Curvilinearly Stiffened Plates Using Ritz Method With Orthogonal Jacobi Polynomials

Journal of vibration and acoustics, 2020-02, Vol.142 (1)

2020

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Structural Optimization of Internal Structure of Aircraft Wings with Curvilinear Spars and Ribs

Journal of aircraft, 2019-03, Vol.56 (2), p.707-718

2019

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Failure of Hexagonal and Triangular Honeycomb Core Sandwich Panels

AIAA journal, 2020-11, Vol.58 (11), p.4923-4940

2020

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Buckling Load Maximization of Curvilinearly Stiffened Tow-Steered Laminates

Journal of aircraft, 2019-11, Vol.56 (6), p.2272-2284

2019

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Single Cell Forces after Electroporation

ACS nano, 2021-02, Vol.15 (2), p.2554-2568

2021

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Up to lowest 100 frequencies of rectangular plates using Jacobi polynomials and TSNDT

Journal of sound and vibration, 2020-08, Vol.480, p.115352, Article 115352

2020

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Free Vibration of Thick Quadrilateral Laminates Using Third-Order Shear-Normal Deformation Theory

AIAA journal, 2020-10, Vol.58 (10), p.4580-4594

2020

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

Engineering optimization, 2020-09, Vol.52 (9), p.1561-1587

2020

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Prestressed Vibration of Stiffened Variable-Angle Tow Laminated Plates

Topology optimization with advanced CNN using mapped physics-based data

Development of Deep Convolutional Neural Network for Structural Topology Optimization

Comparative Study of Skin–Stringer Connection Approaches for Stiffened Structures with Curvilinear Stiffeners

Isogeometric Thermal Buckling and Sensitivity Analysis of Periodically Supported Laminated Composite Beams

Bilevel Programming Weight Minimization of Composite Flying-Wing Aircraft with Curvilinear Spars and Ribs

Tire mode shape categorization using Zernike annular moment and machine learning classification

ALGA: Active Learning-Based Genetic Algorithm for Accelerating Structural Optimization

Thermal Buckling Analysis and Optimization of Curvilinearly Stiffened Plates with Variable Angle Tow Laminates

Buckling and Prestressed Vibrations of Periodic Nonprismatic Beams Using Integral Equation Approach

Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization

Optimization of Hybrid Composite Laminates with Distinct Ply Thicknesses Using Integer Programming

Skin-Stringer Assembly Using Radial Basis Functions for Curvilinearly Stiffened Panels

Two-Level Weight Optimization of Composite Laminates Using Integer Programming

Vibration Analysis of Curvilinearly Stiffened Composite Panel Subjected to In-Plane Loads

A sensitivity-based nonlinear finite element model updating method for nonlinear engineering structures

Global/Local Optimization of Aircraft Wing Using Parallel Processing

Vibration of Curvilinearly Stiffened Plates Using Ritz Method With Orthogonal Jacobi Polynomials

Structural Optimization of Internal Structure of Aircraft Wings with Curvilinear Spars and Ribs

Failure of Hexagonal and Triangular Honeycomb Core Sandwich Panels

Buckling Load Maximization of Curvilinearly Stiffened Tow-Steered Laminates

Single Cell Forces after Electroporation

Up to lowest 100 frequencies of rectangular plates using Jacobi polynomials and TSNDT

Free Vibration of Thick Quadrilateral Laminates Using Third-Order Shear-Normal Deformation Theory

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

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