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|a9780081009697 (electronic bk.)
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|a0081009690 (electronic bk.)
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|a008100964X (hbk.)
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|a9780081009642
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|aTL672
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|aMorphing wing technologies|h[electronic resource] :|blarge commercial aircraft and civil helicopters /|cedited by Antonio Concilio, Ignazio Dimino, Leonardo Lecce, Rosario Pecora.
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|aFirst edition.
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|aCambridge, MA :|bButterworth-Heinemann,|c2018.
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|a1 online resource :|bcol. ill.
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|aIncludes index.
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|aIncludes bibliographical references at the end of each chapters and index.
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|gMachine generated contents note:|gch. 1|tHistorical Background and Current Scenario --|g1.|tIntroduction --|g2.|tComponents of a Wing Morphing Structural System --|g2.1.|tStructural Skeleton --|g2.2.|tActuation Systems --|g2.3.|tSkin --|g2.4.|tControl System --|g2.5.|tCabling --|g2.6.|tAssembly --|g3.|tMain Challenges --|g3.1.|tSkins --|g3.2.|tActuation Systems --|g3.3.|tSensor Systems --|g4.|tBack to the Past --|g4.1.|tWright's Flyer --|g4.2.|tPlane and the Like for Aeroplanes --|g4.3.|tParker's Wing --|g5.|tModern Times --|g5.1.|tNASA Studies --|g5.2.|tDGLR Studies --|g5.3.|tMission Adaptive Wing --|g5.4.|tFurther NASA Studies --|g6.|tRecent Activities-United States --|g6.1.|tAdaptive Wing Reborn: SMAs --|g6.2.|tDARPA Smart Wing Program --|g6.3.|tDARPA Morphing Aircraft Structures Program --|g7.|tRecent Activities-Europe --|g7.1.|tADIF --|g7.2.|tClean Sky --|g8.|tCurrent Scenario --|g8.1.|tAirbus-SARISTU (Smart Intelligent Aircraft Structures) --|g8.2.|tBoeing-Adaptive Wing --|g8.3.|tFlexsys and Gulfstream --|g9.|tTradition at the University of Napoli and CIRA --|g9.1.|tAdaptive Airfoil --|g9.2.|tHinge-Less Wing --|g9.3.|tSmartflap --|g9.4.|tSADE --|g9.5.|tClean Sky-JTI-GRA-Low Noise --|g9.6.|tEU-SARISTU --|g9.7.|tAdaptive Aileron --|g10.|tFuture Perspectives --|g10.1.|tSafe Design --|g10.2.|tSkins and Fillers --|g10.3.|tDirect Actuation: The Use of Smart Materials --|g10.4.|tWireless, Distributed Sensing --|g10.5.|tControl System Architecture --|g10.6.|tCybernetics and Robotics --|tAcknowledgments --|tReferences --|tUniversity of Napoli and CIRA International Awards --|gch. 2|tAircraft Morphing-An Industry Vision --|g1.|tIntroduction --|g2.|tCurrent Aircraft Capabilities --|g2.1.|tInterest of Industry --|g2.2.|tSome Considerations About Industry Aerodynamic Design Process --|g2.3.|tExpected Performance Targets --|g2.4.|tManufacturing: New Materials and Controlled Industrial Processes --|g2.5.|tAssembly and Quality: Automation and Integrated Parts --|g2.6.|tMaintenance: Assessed Steps and Personnel Training --|g2.7.|tSafety: Assessed Methods for Standard Architectures --|g3.|tCurrent and Expected Needs --|g3.1.|tTechnology Transition --|g3.2.|tMission Configurable Wing --|g3.3.|tImproved Flaps and Ailerons --|g4.|tMorphing as a Solution --|g4.1.|tWing and Control Surface Feasible Solutions --|g4.2.|tSome Specific Requirements --|g5.|tConclusions --|tReferences --|gch. 3|tDevelopment of Morphing Aircraft Benefit Assessment --|g1.|tExperiments as Basis for Morphing Progress --|g2.|tAdvent of Transonic Methods --|g3.|tAutomated Methods as Enabler for Large Scale Studies --|g4.|tReintroduction of Flexible Materials --|g5.|tFinal Step to Industrial Application --|tReferences --|gch. 4|tSpan Morphing Concept: An Overview --|g1.|tIntroduction --|g2.|tEffects of Span Increase --|g2.1.|tAerodynamic Effects --|g2.2.|tStructural Effects --|g2.3.|tStability and Control Effects --|g3.|tSpan Morphing Concepts and Aircraft Performance --|g3.1.|tSymmetric Span Morphing --|g3.2.|tAsymmetric Span Morphing --|g4.|tImplementation Challenges --|g4.1.|tTelescopic Wings --|g4.2.|tHinged Structures --|g4.3.|tTwin Spars --|g5.|tConclusions --|tAcknowledgments --|tReferences --|gch. 5|tAdjoint-Based Aerodynamic Shape Optimization Applied to Morphing Technology on a Regional Aircraft Wing --|g1.|tIntroduction --|g2.|tHandling of Morphing Shape Changes in a CFD Context --|g2.1.|tContext of the Study --|g2.2.|tDiscrete Model of Displacement Field at the Trailing Edge --|g2.3.|t3D CFD Mesh Deformation Technique --|g3.|tCFD Evaluation and Far-Field Drag Analysis Over a Wing Equipped with a Morphing System --|g3.1.|tFinite-Volume Solver for the RANS Equations in elsA --|g3.2.|tFar-Field Drag Extraction Tool --|g4.|tSensitivity Analysis Using a Discrete Adjoint of the RANS Equations --|g4.1.|tResidual and Objective Function Dependencies --|g4.2.|tDiscrete Adjoint Method in elsA --|g5.|tLocal Shape Optimization Technique --|g5.1.|tDefinition of the Problem --|g5.2.|tMethod of Feasible Directions --|g5.3.|t2D Example: The Rosenbrock's Function Constrained by a Disk --|g6.|tAerodynamic Shape Optimization of Morphing System: An Application Within the EU Project SARISTU --|g6.1.|tOptimization Problem --|g6.2.|tOptimization Loop Presentation --|g6.3.|tFirst Optimization --|g6.4.|tSecond Optimization --|g6.5.|tExpectations on Morphing Technology --|g7.|tConclusion --|tReferences --|tFurther Reading --|gch. 6|tExpected Performances --|g1.|tIntroduction --|g2.|tReference Aircraft --|g3.|tActive Camber Using Conventional Control Surfaces --|g3.1.|tFive Panels Over the Flap Region --|g4.|tCoupled Aerostructural Shape Optimization --|g4.1.|tMorphing Leading Edge --|g4.2.|tMorphing Trailing Edge --|g5.|tFuel Savings --|g6.|tHigh-Fidelity Aerodynamic Analysis --|g6.1.|tLeading Edge Morphing --|g6.2.|tTrailing Edge Morphing --|g7.|tWeight Saving --|g7.1.|tMorphing Devices --|g8.|tBenefit Exploitation in the Transport Aircraft Design --|g9.|tConclusions --|tAcknowledgments --|tReferences --|gch. 7|tMorphing Skin: Foams --|g1.|tIntroduction --|g2.|tDesign Principles --|g3.|tLow Temperature Elastomers --|g4.|tMaterial Properties of HYPERFLEX --|g5.|tProperties of Bonded Joints --|g6.|tProperties of Morphing Skin --|g7.|tSkin Manufacturing --|g8.|tSummary and Conclusions --|tReferences --|gch. 8|tDesign of Skin Panels for Morphing Wings in Lattice Materials --|g1.|tIntroduction --|g2.|tRequirements for the Skin of a Morphing Wing --|g3.|tMethodology for Nonlinear Homogenization of Periodic Structures --|g4.|tMechanical Properties of Skin Panels in Lattice Material --|g4.1.|tAnalysis of Selected Lattice Topologies --|g4.2.|tDesign Space of the Chevron Lattice --|g5.|tConclusions --|tReferences --|gch. 9|tComposite Corrugated Laminates for Morphing Applications --|g1.|tIntroduction --|g2.|tTypes of Corrugated Laminates --|g3.|tAnisotropy and Stiffness Properties in Morphing Direction --|g3.1.|tAnisotropy Indices of Stiffness Properties --|g3.2.|tCompliance in Morphing Directions of Different Types of Composite Corrugated Laminates --|g4.|tStrength and Stiffness Contributions in Nonmorphing Directions --|g4.1.|tFailure Modes of Composite Corrugated Laminates and Strain Limits --|g4.2.|tEvaluation of Structural Stiffness Contribution in Nonmorphing Directions --|g5.|tManufacturing of Composite Corrugated Laminates --|g6.|tDevelopment of Aerodynamically Efficient Morphing Skins --|g6.1.|tAerodynamic Issues in the Application of Composite Corrugated Laminates --|g6.2.|tPerformance Index Based on Ratio Between Bending and Axial Compliance --|g6.3.|tIntegration of an Elastomertic Cover on a Square-Shaped Corrugated Laminate --|g7.|tConclusions --|tReferences --|gch. 10|tActive Metal Structures --|g1.|tIntroduction --|g2.|tMorphing Oriented Kinematic Chains: Working Principles and Design Approaches --|g2.1.|tSpar Caps Section Area at Generic Cross-section --|g2.2.|tSpars Webs, Skin Panels, Rib Plate Thickness at Generic Cross-Section --|g3.|tCompliant Mechanisms: Working Principles and Design Approaches --|g4.|tApplications of Morphing Oriented Kinematic Chains --|g4.1.|tMorphing Concept Overview --|g4.2.|tStructural Analyses --|g5.|tApplications of the Compliant Mechanism Approach --|g5.1.|tArc-Based Flap, Actuated by SMA Active Elements --|g5.2.|tX-Cell Architecture for a Single Slotted Flap --|g6.|tConclusions --|tReferences --|gch.
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|t11|tSensor Systems for Smart Architectures --|g1.|tIntroduction --|g2.|tStrain Sensors --|g2.1.|tStrain Gauge Foils --|g2.2.|tPiezoelectric Devices --|g2.3.|tGraphene-Based Polymers --|g2.4.|tFiber Optics --|g3.|tSensor Systems for Large Scale Integration --|g3.1.|tWireless Technology --|g3.2.|tSprayed Technology --|g3.3.|tDistributed Technology --|g3.4.|tSome Installation Issues --|g4.|tCase Studies --|g4.1.|tShape Reconstruction of a Variable Camber Wing Trailing Edge --|g4.2.|tDamage and Load Monitoring --|g4.3.|tRotation Angle Monitoring --|g5.|tConclusions and Perspectives --|tReferences --|gch. 12|tControl Techniques for a Smart Actuated Morphing Wing Model: Design, Numerical Simulation and Experimental Validation --|g1.|tIntroduction --|g2.|tProject Background --|g3.|tGeneral Structures of the Open Loop and Closed Loop Control Architectures --|g4.|tOpen Loop Controllers --|g4.1.|tFuzzy Logic PD Controller --|g4.2.|tCombined On-Off and PID Fuzzy Logic Controller --|g4.3.|tCombined On-Off and Cascade PD-PI Fuzzy Logic Controller --|g4.4.|tCombined On-Off and Self-Tuning Fuzzy Logic Controller --|g5.|tOptimized Closed Loop Control Method --|g6.|tConclusions --|tAcknowledgments --|tReferences --|gch. 13|tInfluence of the Elastic Constraint on the Functionality of Integrated Morphing Devices --|g1.|tIntroduction --|g2.|tFeatures of the FE Models --|g2.1.|tLE Modeling Strategy --|g2.2.|tTE Modeling Strategy --|g2.3.|tWL Modeling Strategy --|g3.|tIsolated Devices Behavior --|g4.|tGlobal Stiffness of the Outer Wing Box --|g5.|tEffects of the Actuation of the Morphing Devices --|g5.1.|tCross Effects --|g5.2.|tEffects on the Wing Box --|g6.|tConclusions and Further Steps --|tReferences --|gch. 14|tApplication of the Extra-Modes Method to the Aeroelastic Analysis of Morphing Wing Structures --|g1.|tIntroduction --|g2.|tAeroelastic Equilibrium Equation and Stability --|g3.|tExtra-Modes Formulation --|g4.|tAeroelastic Analyses of Morphing Wings Using the Extra-Modes Method --|g4.1.|tEffectiveness of Wing Twist Morphing as Roll Control Strategy --|g4.2.|tTrade-Off Flutter Analysis of a Morphing Wing Trailing Edge --|g5.|tConclusions --|tBibliography --|gch. 15|tStress Analysis of a Morphing System --|g1.|tIntroduction --|g2.|tDesign of a Morphing Structure.
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|gNote continued:|g3.|tFinite Element Modeling of Morphing Structures --|g3.1.|tRib and Spars --|g3.2.|tFasteners --|g3.3.|tSkin --|g3.4.|tActuation System --|g4.|tDesign Loads and Constraints --|g5.|tStructural Design and Simulations --|g5.1.|tStatic Analysis at Limit and Ultimate Loads: Linear and Nonlinear Analysis --|g5.2.|tStress Analysis --|g5.3.|tBuckling Analysis --|g5.4.|tModal Analysis --|g6.|tStress Margins of Safety --|g6.1.|tSolid Parts --|g6.2.|tInternal Connections --|g7.|tConclusions --|tReferences --|tFurther Readings --|gch. 16|tMorphing of the Leading Edge --|g1.|tSummary --|g2.|tIntroduction --|g3.|tConceptual Approach to the Morphing of the Leading Edge --|g4.|tWorking Principle of the Architecture Selected to Produce the Drop Nose Effect --|g5.|tArchitecture Design --|g5.1.|tIdentification of the Kinematic Chain in the Rib Plane --|g5.2.|tTopologic Optimization of the In-Plane Rib Architecture --|g5.3.|tSpanwise Architecture and Actuation Design --|g5.4.|tModelling and Working Simulation of the Complete Architecture --|g6.|tPrototyping --|g7.|tExperimental Campaign --|g7.1.|tSetup --|g7.2.|tExperimental Results --|g7.3.|tNumerical-Experimental Comparison --|g8.|tConclusions and Further Steps --|tReferences --|gch. 17|tAdaptive Trailing Edge --|g1.|tIntroduction --|g2.|tConcept --|g2.1.|tLayout --|g3.|tDesign --|g3.1.|tDesign Loads --|g3.2.|tStructural Sizing --|g3.3.|tActuator Selection --|g3.4.|tResults --|g4.|tSafety and Reliability Aspects --|g4.1.|tGeneralities --|g4.2.|tDistributed Actuation --|g4.3.|tATED Function --|g4.4.|tFault Hazard Assessment --|g4.5.|tFunctional Hazard Assessment --|g5.|tDiscussion: Implementation on Real Aircraft --|g5.1.|tSystem Development --|g5.2.|tOperational Aspects --|g5.3.|tAeroelastic Issues --|g6.|tConclusions and Future Developments --|tAcknowledgments --|tReferences --|tFurther Reading --|gch. 18|tMorphing Aileron --|g1.|tIntroduction --|g2.|tConceptual Approach --|g3.|tWorking Principle and T/A Architecture --|g4.|tActuation System Design --|g5.|tNumerical Simulations --|g5.1.|tInterface Load --|g6.|tPrototyping --|g7.|tExperimental Tests and Main Outcome --|g7.1.|tGVT and Numerical Correlation --|g7.2.|tFunctionality Test --|g7.3.|tExperimental Shapes --|g8.|tWind Tunnel Tests --|g9.|tConclusions --|tReferences --|gch. 19|tMorphing Technology for Advanced Future Commercial Aircrafts --|g1.|tIntroduction --|g2.|tATED Manufacturing --|g2.1.|tMorphing System --|g2.2.|tManufacturing --|g2.3.|tAssembly --|g2.4.|tTest Campaign --|g2.5.|tConclusions --|g3.|tOther Experiences --|g3.1.|t3AS Project --|g3.2.|tCURVED Project --|g4.|tFuture Studies-The Morphing Rudder --|g4.1.|tSynthesis --|g4.2.|tManufacturing Challenges --|g4.3.|tLateral Directional Stability Analysis --|g5.|tConclusions --|tReferences --|tFurther Reading --|gch. 20|tMorphing Wing Integration --|g1.|tIntroduction --|g2.|tDemonstrator Components --|g2.1.|tWing Box Primary Structure --|g2.2.|tLeading Edge --|g2.3.|tTrailing Edge --|g2.4.|tWinglet --|g3.|tConditions of Assembly --|g4.|tJig --|g5.|tEquipment and Tooling --|g6.|tDemonstrator Assembly --|g6.1.|tAssembly of the Wing Box --|g6.2.|tMorphing Systems Installation: The Leading Edge --|g6.3.|tMorphing Systems Installation: The Trailing Edge --|g6.4.|tMorphing Systems Installation: The Winglet --|g7.|tFBG Sensor Network --|g8.|tConclusions --|tAcknowledgments --|tReferences --|gch. 21|tMorphing Devices: Safety, Reliability, and Certification Prospects --|g1.|tIntroduction --|g2.|tSystem Level Approaches to the Certification of Morphing Wing Devices --|g2.1.|tAdaptive Droop Nose --|g2.2.|tAdaptive Trailing Edge Device --|g2.3.|tMorphing Winglet --|g2.4.|tDefining the System Level Functions of Morphing Devices --|g2.5.|tDual Level Safety --|g3.|tFunctional Hazard Assessment --|g4.|tDual-Level Approach for the FTA of a Morphing Wing --|g5.|tCommon Cause Analyses --|g5.1.|tParticular Risk Analysis --|g5.2.|tCommon Mode Analysis --|g5.3.|tZonal Safety Analysis --|g6.|tConclusions --|tReferences --|gch. 22|tOn the Experimental Characterization of Morphing Structures --|g1.|tIntroduction --|g2.|tTesting Practices for Morphing Systems --|g2.1.|tMorphing Trailing Edge Device --|g3.|tUnit Tests: From Component to Morphing System Verification --|g3.1.|tSkin Over Dummy --|g3.2.|tActuators Over Dummy --|g3.3.|tControl System Over Dummy --|g3.4.|tControl System Over Skinned Dummy --|g3.5.|tComplete System --|g4.|tSystem Integration Test Bench for Morphing Systems --|g5.|tFull-Scale Testing --|g5.1.|tShape Control of Adaptive Wings --|g5.2.|tWing Shape Controller Strategies and Experimental Verification --|g6.|tConclusions --|tReferences --|gch. 23|tWind Tunnel Testing of Adaptive Wing Structures --|g1.|tIntroduction --|g1.1.|tGeneral Test Procedure for the Morphing Item --|g2.|t3AS --|g2.1.|tRequirements for the EURAM and Experimental Facilities --|g2.2.|tModel Design and Manufacture --|g2.3.|tLaboratory Tests --|g2.4.|tAeroelastic Wing Tip Controls Concept --|g2.5.|tAll-Movable Vertical Tail Concept --|g2.6.|tSelective Deformable Structure Concept --|g3.|tSADE --|g3.1.|tWing Demonstrator --|g3.2.|tVideogrammetry Method of Deformation Measuring --|g3.3.|tTest Object and Experimental Facility --|g3.4.|tMeasuring Process and Data Handling --|g4.|tSARISTU --|g4.1.|tObjectives of the Wind Tunnel Test --|g4.2.|tGround Vibration Test and Flutter Expansion Test --|g4.3.|tLoad Measurements --|g4.4.|tCalculations of Wing Demo Aerodynamics in T-104 WT --|g4.5.|tDeformations Measurements of the Wing with Elastic Controls in WT T-104 Flow --|g5.|tConclusions --|tAcknowledgments --|tReferences --|gch. 24|tRotary Wings Morphing Technologies: State of the Art and Perspectives --|g1.|tIntroduction --|g2.|tOverview of Rotor Morphing Technologies --|g2.1.|tTrailing Edge Flaps --|g2.2.|tActive and Variable Twist --|g2.3.|tVariable Span --|g2.4.|tEmerging Rotor Morphing Technologies --|g3.|tCritical Review of Some Significant Efforts --|g3.1.|tActive Trailing and Leading Edge Devices --|g3.2.|tIndividual Blade Control --|g3.3.|tActive Twist --|g3.4.|tVariable Span --|g3.5.|tSlowed/Stopped Rotor --|g4.|tConclusions --|tReferences --|gch. 25|tAerodynamic Analyses of Tiltrotor Morphing Blades --|g1.|tIntroduction --|g2.|tAim and Structure of the Chapter --|g3.|tResearch Context --|g4.|tOutline of Methods and Numerical Tools --|g4.1.|tIntegration and Optimization Environment --|g4.2.|tMDA Procedures and Optimization Processes --|g4.3.|tBEMT Analysis --|g4.4.|tCFD Driven Analysis --|g4.5.|tBlade Parameterization --|g4.6.|tAirfoil Selection --|g4.7.|tSurface Grid Generation --|g4.8.|tVolume Grid Generation --|g5.|tBackground --|g6.|tCase Study --|g6.1.|tDescription of Activities --|g6.2.|tBaseline Geometry --|g6.3.|tOptimization Objectives and Strategy --|g7.|tUn-Morphed Blades --|g8.|tMorphing Blades --|g8.1.|tBlade Span Morphing and Variable Speed Rotor --|g8.2.|tBlade Section Morphing --|g9.|tConclusions --|tReferences --|gch. 26|tSynergic Effects of Passive and Active Ice Protection Systems --|g1.|tIntroduction --|g2.|tPros and Cons of Considered IPS --|g2.1.|tThermoelectric IPS --|g2.2.|tLow-Power Consuming Piezoelectric Deicing Systems --|g2.3.|tHydrophobic Coatings --|g2.4.|tAlternative Strategy Based on a Hybrid Approach --|g3.|tDesign and Realization of the IPS --|g3.1.|tHydrophobic Coating Design and Process Assessment --|g3.2.|tThermoelectric System Design and Ice Shedding Prediction --|g3.3.|tPiezoelectric IPS Sizing and Parameters Assessment --|g4.|tExperimental Validation --|g4.1.|tFirst WT Test Campaign --|g4.2.|tSecond WT Test Campaign --|g5.|tConclusions --|tAcknowledgment --|tReferences --|tFurther Reading --|gch.
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|t27|tHelicopter Vibration Reduction --|g1.|tIntroduction --|g2.|tNextGen Vibration Levels --|g3.|tVibration Specifications --|g4.|tSource of Helicopter Vibratory Loads --|g5.|tHow Do Vibratory Loads Get Into the Fuselage? --|g6.|tWhat Is Used for Vibration Control Now? --|g6.1.|tWhy Not Isolation? --|g6.2.|tVenerable Frahm --|g6.3.|tFuselage-Based Frahms --|g6.4.|tRotor-Based Frahms --|g6.5.|tFrahms Are Heavy --|g6.6.|tActive Vibration Control --|g6.7.|tDynamic Antiresonant Vibration Isolator --|g7.|tMore Problems With Frahms --|g8.|tActive Counter-Force --|g8.1.|tHigher Harmonic Control --|g9.|tIndividual Blade Control --|g9.1.|tHydraulic IBC --|g9.2.|tElectrical IBC --|g9.3.|tOn-Blade Flaps --|g10.|tPath Forward --|tAcknowledgments --|tReferences.
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|aMorphing Wings Technologies: Large Commercial Aircraft and Civil Helicopters offers a fresh look at current research on morphing aircraft, including industry design, real manufactured prototypes and certification. This is an invaluable reference for students in the aeronautics and aerospace fields who need an introduction to the morphing discipline, as well as senior professionals seeking exposure to morphing potentialities. Practical applications of morphing devices are presented-from the challenge of conceptual design incorporating both structural and aerodynamic studies, to the most promising and potentially flyable solutions aimed at improving the performance of commercial aircraft and UAVs. Morphing aircraft are multi-role aircraft that change their external shape substantially to adapt to a changing mission environment during flight. The book consists of eight sections as well as an appendix which contains both updates on main systems evolution (skin, structure, actuator, sensor, and control systems) and a survey on the most significant achievements of integrated systems for large commercial aircraft.
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|aOnline resource; title from PDF title page (Ebsco, viewed October 25, 2017).
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650 |
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|aAirplanes|xWings|xDesign.
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0
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|aVertically rising aircraft|xWings|xDesign.
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7
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|aTECHNOLOGY & ENGINEERING|xEngineering (General)|2bisacsh
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7
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|aAirplanes|xWings|xDesign.|2fast|0(OCoLC)fst00803549
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655 |
4
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|aElectronic books.
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700 |
1
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|aConcilio, Antonio,|d1964-
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700 |
1
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|aDimino, Ignazio.
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1
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|aLecce, Leonardo.
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700 |
1
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|aPecora, Rosario.
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40
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|uhttps://www.sciencedirect.com/science/book/9780081009642
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