American Institute of Aeronautics and Astronautics, Reston, Virginia, 2010. 473 p. — ISBN: 978-1-60086-725-5.
This book presents results from a major European research project, Value Improvement through a Virtual Aeronautical Collaborative Enterprise (VIVACE), on the collaborative civil aeronautical enterprise. In this context the virtual product refers to all components that comprise an aircraft, the structure, the systems, and the engines. The book structure follows the phases of a generic design cycle, beginning with chapters covering Multidisciplinary Design Optimization (MDO) issues at initial design stages and then gradually moving to more detailed design optimization. The MDO applications are ordered by product complexity, from whole aircraft and engine to single component optimization. Final chapters focus on engineering data management, product life cycle management, security, and automated workflows. Inspired and verified by real industrial use cases, the innovative methods and infrastructure solutions contained in this book present a radical step forward toward the advancement, industrialization, and standardization of the MDO concept and will benefit researchers and practitioners in the field of complex systems design.
OverviewErnst Kesseler, Katern 09, Amsterdam, The Netherlands; and Marin D. Guenov, Cranfield University, Bedfordshire, England, United Kingdom
European Industry-Led Research Collaboration
Project Objectives
Outline of the Book
MDO at Predesign StageMarin D. Guenov, Paolo Fantini, Libish Balachandran, Jeremy Maginot, and Mattia Padulo, Cranfield University, Cranfield, England, United Kingdom
Nomenclature
Computational Workflow Management
Multi-Objective Optimization
Sensitivity Analysis
Design Robustness
Results
Helicopter Predesign Strategy: Design-to-Mass or Design-to-Cost?Jos Stevens and Jan-Floris Boer, National Aerospace Laboratory (NLR), Amsterdam, The Netherlands; Cyrille Sevin, Eurocopter SaS, Marignane, France; and Jos Vankan and Wim Lammen, National Aerospace Laboratory (NLR), Amsterdam, The Netherlands
Nomenclature
Rotorcraft Analysis Tool
Specification of Requirements
Predesign Methodology
Analysis Features
Life-Cycle-Cost Model
Life-Cycle-Cost Model in Predesign Analysis Tool
Optimization Methodology
Concluding Remarks
Aeroelasticity and Sizing in a Multilevel ModelingApproach for Preliminary Design
Wolf R. Kru¨ger, German Aerospace Center, Go ¨ttingen, Germany; Anja Wetzel, German Aerospace Center, Braunschweig, Germany; Martin Spieck, German
Aerospace Center, Go¨ttingen, Germany; and Jens Baaran, German Aerospace
Center, Braunschweig, Germany
Nomenclature
Motivation
Basis Considerations for a Modular Framework for Preliminary Design
Simulation Toolbox — an Application of a Module for Multidisciplinary Design
Example: Structural Sizing of a Transport Aircraft Wing
Results of the Simulation and Sizing Process Loops
Summary and Outlook
Multidisciplinary Wing Design OptimizationMartin Laban and Paul Arendsen, National Aerospace Laboratory (NLR), Amsterdam, The Netherlands
Nomenclature
Wing MDO Framework Architecture
Parametric Geometry Generation
Weight and Balance
Structural Wing-Box Optimization
Aerodynamics
Engine Sizing
Flight Mechanics
Mission Analysis
Meta-Modeling and Multi-Objective Optimization in Aeronautic MDOW. J. Vankan, W. Lammen, and R. Maas, National Aerospace Laboratory
(NLR), Amsterdam, The Netherlands
Introduction — MDA, MDO, and MOO in Aeronautics
Meta-Modeling
Optimization — MDA, MDO, and MOO in Aeronautics
Case Study: Multi-Objective Optimization of Transonic
Wing Design
Fuselage Structure OptimizationSte´phane Grihon, AIRBUS, Toulouse, France; Manuel Samuelides and Antoine Merval, ONERA, Toulouse, France; Alain Remouchamps, Michael Bruyneel, and Benoit Colson, SAMTECH, Lie`ge, Belgium; and Klaus Hertel, AIRBUS, Bremen, Germany
Nomenclature
Presentation of the Test Case
Local Optimization
Integration
Tight Coupling
Loose Coupling
Additional Considerations
Refinement of Local Optimization
Summary and Conclusions
Pylon Multidisciplinary OptimizationSt´phane Grihon, Mathieu Meaux, Albert Lucchetti, and Patrick Sarouille, AIRBUS, Toulouse, France; Julien Laurenceau, CERFACS, Toulouse, France; and Ge´rald Carrier and Sylvain Mouton, ONERA, Paris, France
Nomenclature
Presentation of the Test Case
Single Discipline Optimizations
Integration of Stress and Aerodynamic Optimization
Integration of Stress and Loads Optimization
Summary and Conclusions
Engine MDO Deployed on a Two-Stage TurbineRoland Parchem and Bernd Meissner, Rolls-Royce Deutschland, Dahlewitz, Germany; Marc Nagel, MTU, Munich, Germany; and Ernst Kesseler, Katern 09, Amsterdam, The Netherlands
Nomenclature
Requirements for Engine MDO and Robust Design in the Virtual Enterprise
Realization of the Engine MDO and RD in the Virtual Enterprise
MDO at Airfoil Design Partner in Munich, Germany
High-Pressure Turbine Disc Assembly Design Optimization
Design Framework Used at Disc Design Partner in Berlin
Design Framework Used at Disc Partner in Amsterdam
Using the Virtual-Enterprise-Collaboration Hub for Distributed Engine OptimizationHolger Wenzel, Engineous Software GmbH, Aachen, Germany; Fredrik Almyren, Volvo Aero Corporation, Trollha ¨ ttan, Sweden; Johannes Barner, MTU Aero Engines, Munich, Germany; Erik Baalbergen, National Aerospace Laboratory (NLR), Amsterdam, The Netherlands; Bernd Meissner, Rolls-Royce Deutschl and Dahlewitz, Germany; and Mats Lindeblad, Volvo Aero Corporation,
Trollha¨ttan, Sweden
Description of the VEC Hub
Global Optimization Workflow
Connection to the DDP
Connection to the Turbine Life Assessment Partner
Summary and Conclusions
Securing Virtual-Enterprise CollaborationMichel Kamel, Paul Sabatier University, IRIT, Toulouse, France; Ernst Kesseler, Katern 09, Amsterdam, The Netherlands; Jean Paul Buu-Sao, Transglobal
Secure Collaboration Program, Toulouse, France; Abdelmalek Benzekri, Paul Sabatier University, IRIT, Toulouse, France; Rene Wiegers, National Aerospace Laboratory (NLR), Amsterdam, The Netherlands; Franc¸ois Barrere, Paul Sabatier University, IRIT, Toulouse, France; Bert Schultheiss, National
Aerospace Laboratory (NLR), Amsterdam, The Netherlands; Romain Laborde,
Paul Sabatier University, IRIT, Toulouse, France; and Erik H. Baalbergen,
National Aerospace Laboratory (NLR), Amsterdam, The Netherlands Trust
Collaborative Environments and Security Constraints
Access Control Architecture Proposal
Workflow Engine Descriptive Scenario
Prototype
Enhancing the Access Control Solution
Securing the Virtual-Enterprise Collaboration Hub
Appendix: Description of a Logical Connective
EDMRF to Ensure Partners’ Collaboration for Multidisciplinary OptimizationFrederic Fe ´ru, EADS, France; Thomas Nguyen Van and Pierre-Laurent Frossard, Snecma, France; Ernst Kesseler, Katern 09, Amsterdam, The Netherlands; and Pascal Guellec, AIRBUS Cimpa, France
Virtual Enterprise and Collaborative Environments
Technological Guidelines and Drivers
EDM Framework
Scenario Description and Test Case Run
Appendix. VIVACE Partners
Supporting Materials