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Advanced Multifunctional Lightweight Aerostructures -

Advanced Multifunctional Lightweight Aerostructures

Design, Development, and Implementation
Buch | Hardcover
256 Seiten
2021 | 1st ed.
Wiley-Blackwell (Verlag)
978-1-119-75671-2 (ISBN)
CHF 188,65 inkl. MwSt
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Offers a review of the newest methodologies for the characterization and modelling of lightweight materials and structures.
»Advances in Multifunctional Lightweight Structures« offers a text that provides and in-depth analyses of the thermal, electrical and mechanical responses of multi-functional lightweight structures. The authors, noted experts on the topic, address the most recent and innovative methodologies for the characterization and modelling of lightweight materials and discuss various shell and plate theories. They present multifunctional materials and structures and offer detailed descriptions of the complex modelling of these structures.

The text is divided into three sections that demonstrate a keen understanding and awareness for multi-functional lightweight structures by taking a unique approach. The authors explore multi-disciplinary modelling and characterization alongside benchmark problems and applications, topics that are rarely approached in this field. This important book:

  • Offers an analyses of the thermal, electrical and mechanical responses of multi-functional lightweight structures
  • Covers innovative methodologies for the characterization and modelling of lightweight materials and structures
  • Presents a characterization of a wide variety of novel materials
  • Considers multifunctional novel structures with potential applications in different high-tech industries
  • Includes efficient and highly accurate methodologies

Written for professionals, engineers and researchers in industrial and other specialized research institutions, Advances in Multifunctional Lightweight Structures offers a much needed text to the design practices of existing engineering building services and how these methods combine with recent developments.

Dr. Kamran Behdinan, PEng., Professor, Advanced Research Laboratory for Multifunctional Lightweight Structures (ARL-MLS), Department of Mechanical and Industrial Engineering, University of Toronto, Canada. Dr. Rasool Moradi-Dastjerdi, Postdoctoral Fellow, Advanced Research Laboratory for Multifunctional Lightweight Structures (ARL-MLS), Department of Mechanical and Industrial Engineering, University of Toronto, Canada.

1 An overview

2 Multi-disciplinary modelling and characterization

Layer arrangement impact on the electromechanical performance of a five-layer multifunctional smart sandwich plate

  • Introduction
  • Modeling of the smart plate
  • Porous layer
  • Nanocomposite layers
  • Governing
  • Equations
  • Mesh-free solution
  • MLS shape function
  • Discretization of domain
  • Essential boundary conditions
  • Numerical results
  • Validation
  • Static deflections of the smart plate
  • Conclusions
  • References

Heat transfer in advanced sandwich cylinders with graphene-reinforced nanocomposite faces

  • Introduction
  • Modeling of sandwich cylinders
  • Dispersion of graphene sheets
  • Thermal properties
  • Governing thermal equations
  • Mesh-free formulations
  • Results and discussions
  • Thermal conductivity of graphene/PE nanocomposite
    Verification
  • Heat transfer response
  • Conclusions
  • References

Multiscale methods for lightweight structure and material characterization

  • Introduction
  • Overview of Multiscale methodologies and applications
  • Concurrent methods
  • Hierarchical methods
  • Bridging Cell Method
  • Formulation
  • Applications
  • Multiscale modeling of lightweight composites
  • Nano to microscale: bridging cell method
  • Micro to macroscale: cohesive zone modeling
  • Conclusion
  • References

Characterization of Ultra-High Temperature and Polymorphic Ceramics

  • Introduction
  • Crystalline Characterization of Ultra-High Temperature Ceramics
  • Chemical Characterization of a UHTC Composite
  • Polymeric Ceramic Crystalline Characterization
  • Multiscale Characterization of Anatase-Rutile Transformation
  • Conclusion
  • References

Dynamic Modeling and Analysis of Nonlinear Flexible Rotors Supported by Viscoelastic Bearings

  • Introduction
  • Kinematics of flexible spinning shafts
  • Dynamic modeling
  • Free vibration analysis
  • Nonlinear analysis
  • Bearing nonlinearities
  • Conclusions
  • References

3 Aerostructure problems and applications

Design optimization of multifunctional aerospace structures

  • Introduction
  • Multifunctional structures
  • Computational design and optimization
  • Applications
  • Design optimization of a novel NLG shimmy damper
  • Conclusion
  • References

An efficient far-field noise prediction framework towards low-noise landing gear designs for new generations of aircraft

  • Introduction and Background
  • Landing Gear Noise Predictions
  • Numerical Aeroacoustics
  • Issues and Methods
  • Acoustic Analogies
  • Numerical Landing Gear Aeroacoustics
  • Problem Statement and Concluding Remarks
  • Modeling and Numerical Method
  • Hybrid Computational Aeroacoustic Method
  • Near-field Flow Numerical Method
  • Far-field Acoustic Numerical Method
  • Acoustic analogies formulation
  • Ffowcs Williams and Hawkings (FW-H) equation
  • The Motivation of Multiple 2D Simulations Method (M2DSM)
  • Proposed Approach for the LG Far-Field Noise Prediction
  • Implementation of the M2DSM on Two Different Landing Gear Models
  • Two-wheel Nose Landing Gear (2-NLG) Model
  • The 2D CFD setup
  • Acoustic Far-Field Computations
  • The Lower Part of the LAGOON NLG
  • The LAGOON NLG wheels inner-cavities modeling
  • Four-wheel Main Landing Gear (4-MLG) Model
  • The 2D CFD Setup
    Acoustic Far-Field Computations
  • The Lower Part of the RLG
  • Results and Discussions
  • Results for the 2-NLG (LAGOON)
  • The effects of the receiver locations
  • The effects of the acoustic source
  • Results for the wheels' inner-cavities
  • The LAGOON NLG overall far-Field acoustic results
  • Results for the 4-MLG (RLG)
  • The effect of the receiver locations
  • The effects of the acoustic source
  • The Cross-Sections of Axles and Wheels of the RLG
  • The RLG overall far-field acoustic results
  • Summary and Conclusions
  • References

Modeling and Experimentation for the Temperature Prediction of a Serpentine Belt

  • Drive Transmission System in the aviation industry
  • Introduction and importance of thermal model for aviation safety
  • Establishment of belt drive analytical-numerical thermal model
  • Experimental Setup for validation of the belt drive System
  • Result discussion for the accuracy of the belt drive System
  • Conclusion
  • References

Transfer Path Analysis of Aeroengines by Implementing Bond Graph Theory

  • Introduction
  • Background
  • Measuring Interface Loads using Classical TPA Approach
  • Mount Stiffness Measurement Technique
  • Matrix Inversion Method (MIM)
  • Operational Path Analysis (OPA)
  • Operational Path Analysis Theory
  • OPAX Method
  • Global Transfer Direct Transfer (GTDT) TPA Method
  • Bond Graph TPA Method
  • Bond Graph
  • Methodology
  • Developing Bond Graphs
  • Aeroengine Modelling
  • State Space Equation of the Reduced Aeroengine
  • Sample Calculation: Output and Direct Transmissibility Matrices
  • Transmissibility Principle
  • Bond Graph Transfer Function
  • Aeroengine Global Transmissibility Formulation
  • Design Guidelines to Minimize Vibration Transfer
  • Conclusion
  • References

Aeroengine structural health monitoring using bond graph methodology and transmissibility-based analysis

  • Introduction
  • Transfer Function Fundamentals and Applications
  • Bond Graph Transfer Path Analysis Methodology
  • Global transmissibility
  • Direct transmissibility
  • Fundamentals of System
  • Transmissibility Analysis using Bond Graph
  • Methodology
  • Aeroengine Structural Health Monitoring using Transmissibility and TPA
  • Principles
  • Structural damage detection
  • Aeroengine Case study
  • Aeroengine bond graph modelling
  • Aeroengine structural damage detection
  • Structural damage detection protocols and design guidelines
  • Finite Element Analysis of the Aeroengine Model
  • Modelling and verification
  • Conclusion
  • References

Erscheinungsdatum
Reihe/Serie Wiley-ASME Press Series
Verlagsort Hoboken
Sprache englisch
Maße 170 x 244 mm
Gewicht 606 g
Einbandart gebunden
Themenwelt Technik Bauwesen
Technik Maschinenbau
ISBN-10 1-119-75671-5 / 1119756715
ISBN-13 978-1-119-75671-2 / 9781119756712
Zustand Neuware
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