Produktbild: Advanced Multifunctional Lightweight

Advanced Multifunctional Lightweight Design, Development, and Implementation

155,99 €

inkl. gesetzl. MwSt., Versandkostenfrei

Lieferung nach Hause

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

08.02.2021

Herausgeber

Behdinan Kamran + weitere

Verlag

John Wiley & Sons Inc

Seitenzahl

256

Maße (L/B/H)

25/17,5/1,8 cm

Gewicht

595 g

Auflage

1. Auflage

Sprache

Englisch

ISBN

978-1-119-75671-2

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

08.02.2021

Herausgeber

Verlag

John Wiley & Sons Inc

Seitenzahl

256

Maße (L/B/H)

25/17,5/1,8 cm

Gewicht

595 g

Auflage

1. Auflage

Sprache

Englisch

ISBN

978-1-119-75671-2

Herstelleradresse

Libri GmbH
Europaallee 1
36244 Bad Hersfeld
DE

Email: [email protected]

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Die Leseprobe wird geladen.
  • Produktbild: Advanced Multifunctional Lightweight
  • (i) An overview (ii) 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 2 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 3 Dynamic modeling Free vibration analysis Nonlinear analysis Bearing nonlinearities Conclusions References (iii) 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 4 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) 5 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