Introduction to Aircraft Aeroelasticity and Loads.

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Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of v...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Wright, Jan R.
Otros Autores: Cooper, Jonathan E.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Hoboken : Wiley, 2014.
Edición:2nd ed.
Colección:Aerospace Series.
Temas:
Aeroelasticity.
Aéroélasticité.
Aeroelasticity
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Title Page; Copyright Page; Contents; Series Preface; Preface to the Second Edition; Preface to the First Edition; Abbreviations; Introduction; Part I Background Material; Chapter 1 Vibration of Single Degree of Freedom Systems; 1.1 Setting up Equations of Motion for SDoF Systems; 1.1.1 Example: Classical SDoF System; 1.1.2 Example: Aircraft Control Surface; 1.2 Free Vibration of SDoF Systems; 1.2.1 Example: Aircraft Control Surface; 1.3 Forced Vibration of SDoF Systems; 1.4 Harmonic Forced Vibration
  • Frequency Response Functions; 1.4.1 Response to Harmonic Excitation.
  • 1.4.2 Frequency Response Functions1.4.3 Hysteretic (or Structural) Damping; 1.5 Transient/Random Forced Vibration
  • Time Domain Solution; 1.5.1 Analytical Approach; 1.5.2 Principle of Superposition; 1.5.3 Example: Single Cycle of Square Wave Excitation
  • Response Determined by Superposition; 1.5.4 Convolution Approach; 1.5.5 Direct Solution of Ordinary Differential Equations; 1.5.6 Example: Single Cycle of Square Wave Excitation
  • Response Determined by Numerical Integration; 1.6 Transient Forced Vibration
  • Frequency Domain Solution; 1.6.1 Analytical Fourier Transform.
  • 1.6.2 Frequency Domain Response
  • Excitation Relationship1.6.3 Example: Single Cycle of Square Wave Excitation
  • Response Determined via Fourier Transform; 1.7 Random Forced Vibration
  • Frequency Domain Solution; 1.8 Examples; Chapter 2 Vibration of Multiple Degree of Freedom Systems; 2.1 Setting up Equations of Motion; 2.2 Undamped Free Vibration; 2.2.1 Direct Approach; 2.2.2 Eigenvalue Approach; 2.2.3 Example: `Chain-like ́ 2DoF System; 2.3 Damped Free Vibration; 2.3.1 Example: 2DoF `Chain-Like ́ System with Proportional Damping.
  • 2.3.2 Example: 2DoF `Chain-Like ́ System with Non-proportional Damping2.4 Transformation to Modal Coordinates; 2.4.1 Modal Coordinates; 2.4.2 Example: 2DoF `Chain-like ́ System with Proportional Damping; 2.4.3 Example: 2DoF `Chain-like ́ System with Non-proportional Damping; 2.4.4 Mode Shape Normalization; 2.4.5 Meaning of Modal Coordinates; 2.4.6 Dimensions of Modal Coordinates; 2.4.6.1 Consistent Coordinates; 2.4.6.2 Mixed Coordinates; 2.4.7 Model Order Reduction; 2.5 Two-DoF Rigid Aircraft in Heave and Pitch; 2.6 `Free-Free ́ Systems; 2.7 Harmonic Forced Vibration.
  • 2.7.1 Equations in Physical Coordinates2.7.2 Equations in Modal Coordinates; 2.8 Transient/Random Forced Vibration
  • Time Domain Solution; 2.8.1 Analytical Approach; 2.8.2 Convolution Approach; 2.8.3 Solution of Ordinary Differential Equations; 2.9 Transient Forced Vibration
  • Frequency Domain Solution; 2.10 Random Forced Vibration
  • Frequency Domain Solution; 2.11 Examples; Chapter 3 Vibration of Continuous Systems
  • Assumed Shapes Approach; 3.1 Continuous Systems; 3.2 Modelling Continuous Systems; 3.3 Elastic and Flexural Axes; 3.4 Rayleigh-Ritz `Assumed Shapes ́ Method.

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