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Quasi-Three-Dimensional Aerodynamic Solver for Multidisciplinary Design Optimization of Lifting Surfaces

Journal of aircraft, 2014-03, Vol.51 (2), p.547-558

2014

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Weight Indexing for Airfoil Multi-Objective Optimization

Journal of aircraft, 2013-07, Vol.50 (4), p.1046-1059

2013

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Analysis and evaluation of bondline thickness effects on failure load in adhesively bonded structures

Journal of adhesion science and technology, 2001-01, Vol.15 (9), p.1091-1101

2001

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Design "Feasilization" Using Knowledge-Based Engineering and Optimization Techniques

Journal of aircraft, 2007-11, Vol.44 (6), p.1776-1786

2007

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Adjoint-based aerodynamic shape optimization on unstructured meshes

Journal of computational physics, 2007-05, Vol.224 (1), p.267-287

2007

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Multi-Agent Task Environment Framework to Support Multidisciplinary Design and Optimization

Journal of aerospace information systems, 2013-06, Vol.10 (6), p.258-267

2013

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Multidisciplinary Design Optimization Supported by Knowledge Based Engineering

1, 2015

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Development and implementation of an advanced, design-sensitive method for wing weight estimation

Aerospace science and technology, 2013-08, Vol.29 (1), p.100-113

2013

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A methodology to enable automatic 3D routing of aircraft Electrical Wiring Interconnection System

CEAS aeronautical journal, 2017-06, Vol.8 (2), p.287-302

2017

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Parametric Modeling of Movables for Structural Analysis

Journal of aircraft, 2005-11, Vol.42 (6), p.1605-1613

2005

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Knowledge-based engineering to support aircraft multidisciplinary design and optimization

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2010-09, Vol.224 (9), p.1041-1055

2010

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Experimental verification of a stress singularity model to predict the effect of bondline thickness on joint strength

Journal of adhesion science and technology, 2004-01, Vol.18 (4), p.395-412

2004

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Shear and peel stress analysis of an adhesively bonded scarf joint

Journal of adhesion science and technology, 2000-01, Vol.14 (6), p.879-893

2000

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A KBE-enabled design framework for cost/weight optimization study of aircraft composite structures

AIP Conference Proceedings, 2014, Vol.1618 (1), p.397

2014

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Enabling distributed multi-disciplinary design of complex products: a knowledge based engineering approach

Journal of design research (Geneva, Switzerland), 2007, Vol.5 (3), p.333

2007

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Incorporating cost analysis in a multi-disciplinary design environment for aircraft movables

Journal of engineering design, 2008-04, Vol.19 (2), p.131-144

2008

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Application of a knowledge based design methodology to support fuselage panel design

Aeronautical journal, 2010-09, Vol.114 (1159), p.589-597

2010

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Influence of weight modelling on the outcome of wing design using multidisciplinary design optimisation techniques

Aeronautical journal, 2013-09, Vol.117 (1195), p.871-895

2013

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A generalized stress singularity approach for material failure prediction and its application to adhesive joint strength analysis

Journal of adhesion science and technology, 2006-01, Vol.20 (9), p.981-995

2006

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Bubble Bursting and Stall Hysteresis on Single-Slotted Flap High-Lift Configuration

AIAA journal, 2003-07, Vol.41 (7), p.1230-1237

2003

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Design, manufacturing and testing of a fibre steered panel with a large cut-out

Composite structures, 2017-11, Vol.180, p.821-830

2017

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A stress singularity approach to failure initiation in a bonded joint with varying bondline thickness

Journal of adhesion science and technology, 2001-01, Vol.15 (10), p.1247-1259

2001

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Implementation of bending-torsion coupling in the design of a wind-turbine rotor-blade

Applied energy, 1999, Vol.63 (3), p.191-207

1999

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Multi-Disciplinary Design Philosophy for Aircraft Fuselages. Part I

Applied composite materials, 2005-01, Vol.12 (1), p.3-11

2005

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Integration of Mechanics and Acoustics in a Sandwich Fuselage. Part IV

Applied composite materials, 2005-01, Vol.12 (1), p.37-51

2005

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Quasi-Three-Dimensional Aerodynamic Solver for Multidisciplinary Design Optimization of Lifting Surfaces

Weight Indexing for Airfoil Multi-Objective Optimization

Analysis and evaluation of bondline thickness effects on failure load in adhesively bonded structures

Design "Feasilization" Using Knowledge-Based Engineering and Optimization Techniques

Adjoint-based aerodynamic shape optimization on unstructured meshes

Multi-Agent Task Environment Framework to Support Multidisciplinary Design and Optimization

Multidisciplinary Design Optimization Supported by Knowledge Based Engineering

Development and implementation of an advanced, design-sensitive method for wing weight estimation

A methodology to enable automatic 3D routing of aircraft Electrical Wiring Interconnection System

Parametric Modeling of Movables for Structural Analysis

Knowledge-based engineering to support aircraft multidisciplinary design and optimization

Experimental verification of a stress singularity model to predict the effect of bondline thickness on joint strength

Shear and peel stress analysis of an adhesively bonded scarf joint

A KBE-enabled design framework for cost/weight optimization study of aircraft composite structures

Enabling distributed multi-disciplinary design of complex products: a knowledge based engineering approach

Incorporating cost analysis in a multi-disciplinary design environment for aircraft movables

Application of a knowledge based design methodology to support fuselage panel design

Influence of weight modelling on the outcome of wing design using multidisciplinary design optimisation techniques

A generalized stress singularity approach for material failure prediction and its application to adhesive joint strength analysis

Bubble Bursting and Stall Hysteresis on Single-Slotted Flap High-Lift Configuration

Design, manufacturing and testing of a fibre steered panel with a large cut-out

A stress singularity approach to failure initiation in a bonded joint with varying bondline thickness

Implementation of bending-torsion coupling in the design of a wind-turbine rotor-blade

Multi-Disciplinary Design Philosophy for Aircraft Fuselages. Part I

Integration of Mechanics and Acoustics in a Sandwich Fuselage. Part IV

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