rdf-syntax-grammar
mods:
  schema location: http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
  title info:
    title: Modern flexible multi-body dynamics modeling methodology for flapping wing vehicles
  name:
    name part: Altenbuchner, Cornelia
    role:
      role term: creator
    role:
      role term: author.
  name:
    name part: Hubbard, James E., (James Edward)
    name part: Jr
    name part: 1951-
    role:
      role term: author.
  name:
    name part: ScienceDirect (Online service)
  type of resource: text
  genre: bibliography
  genre: Electronic books.
  origin info:
    place:
      place term: enk
    place:
      place term: London
    publisher: Academic Press
    date issued: 2018
    issuance: monographic
  language:
    language term: eng
  physical description:
    form: remote
    extent: 1 online resource : illustrations
  abstract: Modern Flexible Multi-Body Dynamics Modeling Methodology for Flapping Wing Vehicles presents research on the implementation of a flexible multi-body dynamic representation of a flapping wing ornithopter that considers aero-elasticity. This effort brings advances in the understanding of flapping wing flight physics and dynamics that ultimately leads to an improvement in the performance of such flight vehicles, thus reaching their high performance potential. In using this model, it is necessary to reduce body accelerations and forces of an ornithopter vehicle, as well as to improve the aerodynamic performance and enhance flight kinematics and forces which are the design optimization objectives. This book is a useful reference for postgraduates in mechanical engineering and related areas, as well as researchers in the field of multibody dynamics.
  table of contents: Front Cover; MODERN FLEXIBLE MULTI-BODY DYNAMICS MODELING METHODOLOGY FOR FLAPPING WING VEHICLES; MODERN FLEXIBLE MULTI-BODY DYNAMICS MODELING METHODOLOGY FOR FLAPPING WING VEHICLES ; Copyright; Dedication; CONTENTS; PREFACE; LIST OF FIGURES; LIST OF TABLES; LIST OF NOMENCLATURE; ROMAN SYMBOLS; CAPITAL ROMAN SYMBOLS; GREEK SYMBOLS; SUPERSCRIPTS AND SUBSCRIPTS; ACRONYMS; ACKNOWLEDGMENTS; SUMMARY; One -- Bioinspired Flight Robotics Systems; 1.1 INTRODUCTION OF THIS BODY OF WORK; 1.2 THE BACKGROUND OF FLAPPING WING FLIGHT TECHNOLOGY; 1.2.1 Aerial Vehicles and Natural Flapping Wing Flyers.
  table of contents: 1.3 A MODEL OF AN ORNITHOPTER FOR PERFORMANCE OPTIMIZATION1.3.1 Desired Improvements in Flight Platforms; 1.3.2 Background and Flapping Wing Flight Aerodynamics; 1.3.2.1 Motion Profile and Wing Gates; 1.3.2.2 Wing Flexibility; 1.3.2.3 Wing Geometry; 1.4 HISTORICAL CONSIDERATIONS FOR BIOINSPIRED FLAPPING WINGS AVIAN FLIGHT AND ROBOTICS; 1.5 OBJECTIVES IN THE DEVELOPMENT OF FLEXIBLE MULTI-BODY DYNAMICS THE MODELING METHODOLOGY DESCRIBED IN THIS BODY OF WORK; REFERENCES; Two -- Flexible Multi-Body Dynamics Modeling Methodology's for Flapping Wing Vehicles; 2.1 CLASSIC MODELING METHODOLOGY'S.
  table of contents: 2.1.1 The Classification of Flexible Multi-Body Systems2.1.2 Flexible Multi-Body Dynamics Modeling; 2.1.3 The Implementation in Available Code and Software; 2.1.4 The Vehicle Dynamics Modeling of Ornithopter; 2.1.5 An Aeroelastic Analysis of Flapping Wing Vehicles; 2.1.6 Related Avian Scale Aerodynamics and Models; 2.2 MODERN MODELING METHODOLOGY; REFERENCES; Three -- Bioinspired Flapping Wing Test Platform Used to Implement Modern Modeling Methodology; 3.1 DETAILS OF THE TEST PLATFORM; 3.2 EXPERIMENTAL DATA SETS OF BIOINSPIRED FLAPING WING ROBOTIC SYSTEM FOR MODEL VERIFICATION.
  table of contents: 3.2.1 The Clamped Test Experiment-E13.2.1.1 Results of Experiment and Integrated Forces-E1; 3.2.1.2 Wing Kinematics-E-1; 3.2.2 The System-ID Experiment-E1-I; 3.2.2.1 Integrated Aerodynamic Force-E1-I; 3.2.3 Free-Flight Experiment-E2; 3.2.3.1 Results for Wing Kinematics-E-2; 3.2.3.1.1 Total Forces-E2; 3.2.4 Vacuum Camber Experiment-E3; 3.2.4.1 Integrated Inertial Forces-E3; REFERENCES; Four -- Flexible Multi-Body Dynamics Modeling Methodology Implementation Avian Scale Flapping Wing Flyer; 4.1 LINEAR ELASTIC MULTI-BODY SYSTEMS; 4.1.1 A Floating Frame of Reference Formulation.
  table of contents: 4.2 THE FIVE-BODY MULTI-BODY DYNAMICS MODEL4.3 RELEVANT COORDINATE SYSTEMS; 4.4 AN UNDERLYING ARTICULATED RIGID-BODY MODEL; 4.4.1 The Kinematic Relations; 4.4.1.1 Angular Velocity; 4.4.1.2 Linear Velocity; 4.5 LAGRANGE FORMULATION OF EQUATIONS OF MOTION; 4.5.1 Kinetic Energy Formulation; 4.5.2 Potential Energy Formulation; 4.5.3 The Position Vector and Rigid-Body Equations of Motion; 4.5.4 The Position Vector and Flexible Body Equations of Motion; 4.5.5 The Use of Modal Superposition; 4.6 FORMULATION OF FIVE-BODY FLEXIBLE MULTI-BODY DYNAMICS MODEL.
  note: Cornelia Altenbuchner, James E. Hubbard, Jr.
  note: Includes bibliographical references and index.
  subject:
    topic: Aerospace engineering
    topic: Computer simulation
  subject:
    topic: Airplanes
    topic: Wings
  subject:
    topic: Wings (Anatomy)
    topic: Aerodynamics
  subject:
    topic: Vehicles, Remotely piloted
  subject:
    topic: Aérospatiale (Ingénierie)
    topic: Simulation par ordinateur
  subject:
    topic: Avions
    topic: Ailes
  subject:
    topic: Véhicules télécommandés
  subject:
    topic: TECHNOLOGY & ENGINEERING
    topic: Engineering (General)
  subject:
    topic: Airplanes
    topic: Wings
  subject:
    topic: Vehicles, Remotely piloted
  subject:
    topic: Wings (Anatomy)
    topic: Aerodynamics
  classification: TL570
  classification: 629.13230113
  identifier: 9780128141373
  identifier: 0128141379
  identifier: 9780128141366
  identifier: 0128141360
  identifier: http://proxy.library.tamu.edu/login
  record info:
    record content source: YDX
    record creation date: 170920
    record change date: 20260327152419.7
    record identifier: in00005762299
    language of cataloging:
      language term: eng