Structural dynamics in aeronautical engineering

Structural dynamics in aeronautical engineering / Maher N. Bismarck-Nasr.

Annotation "Structural Dynamics in Aeronautical Engineering is a comprehensive introduction to the modern methods of dynamic analysis of aeronautical structures. The text represents carefully developed course materials, beginning with an introductory chapter on matrix algebra and methods for nu...

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Bibliographic Details
Main Author: Bismarck-Nasr, Maher N., 1940-
Format: eBook
Language:English
Published: Reston, Va. : American Institute of Aeronautics and Astronautics, Inc., ©1999.
Series:AIAA education series.
Subjects:
Airframes > Mathematical models.
Space vehicles > Mathematical models.
Structural engineering > Mathematics.
Airframes > Mathematical models
Space vehicles > Mathematical models
Structural engineering > Mathematics
dissertations.
Academic theses
Academic theses.
Thèses et écrits académiques.
Online Access:Click for online access
Table of Contents:
  • Cover
  • Title
  • Copyright
  • Table of Contents
  • Preface
  • Chapter 1. Matrix Algebra and Techniques
  • 1.1 Notations and Definitions
  • 1.2 Matrix Algebra
  • 1.3 Differentiation and Integration of Matrices
  • 1.4 Transformations
  • 1.5 Solution of Large Systems of Linear Equations
  • 1.6 The Eigenvalue Problem
  • References
  • Problems
  • Chapter 2. Single-Degree-of-Freedom Linear Systems
  • 2.1 Equation of Motion
  • 2.2 Free Vibration
  • 2.3 Response to Harmonic Excitation
  • 2.4 Response to an Impulsive Excitation
  • 2.5 Response to a Step Excitation2.6 Response to Periodic Excitation (Fourier Series)
  • 2.7 Response to Aperiodic Excitation (Fourier Transform)
  • 2.8 Laplace Transform (Transfer Function)
  • Problems
  • Chapter 3. Multidegree-of-Freedom Linear Systems
  • 3.1 Equations of Motion
  • 3.2 Free Vibration: The Eigenvalue Problem
  • 3.3 Response to an External Applied Load
  • 3.4 Damping Effect
  • 3.5 Applications
  • References
  • Problems
  • Chapter 4. Dynamics of Continuous Elastic Bodies
  • 4.1 Introduction
  • 4.2 Slender Beams
  • 4.3 Flat Plates
  • 4.4 Shell Structures4.5 Response to Initial Conditions
  • 4.6 Response to External Excitations
  • References
  • Problems
  • Chapter 5. Nonlinear Systems
  • 5.1 Introduction
  • 5.2 Simple Examples of Nonlinear Systems
  • 5.3 Physical Properties of Nonlinear Systems
  • 5.4 Solutions of the Equation of Motion of a Single-Degree-of-Freedom Nonlinear System
  • 5.5 Multidegree-of-Freedom Nonlinear Systems
  • References
  • Problems
  • Chapter 6. Random Vibrations
  • 6.1 Introduction
  • 6.2 Classification of Random Processes
  • 6.3 Probability Distribution and Density Functions6.4 Description of the Mean Values in Terms of the Probability Density Function
  • 6.5 Properties of the Autocorrelation Function
  • 6.6 Power Spectral Density Function
  • 6.7 Properties of the Power Spectral Density Function
  • 6.8 White Noise and Narrow and Large Bandwidth
  • 6.9 Single-Degree-of-Freedom Response
  • 6.10 Response to a White Noise
  • 6.11 Multidegree-of-Freedom Systems
  • References
  • Problems
  • Chapter 7. The Typical Section in Aeroelasticity
  • 7.1 Single-Degree-of-Freedom Stability
  • 7.2 The Typical Section7.3 Typical Section Using Unsteady Linearized Potential Theory
  • 7.4 Typical Section with Control Surface
  • 7.5 Control Surface Reversal and Efficiency
  • References
  • Problems
  • Chapter 8. Aeroelasticity of Flight Vehicles
  • 8.1 Introduction
  • 8.2 Problem Formulation
  • 8.3 Incremental Nonstationary Aerodynamic Loads
  • 8.4 Modal Transformation
  • 8.5 Solution of the Aeroelastic Stability Equations
  • 8.6 Applications
  • 8.7 Optimization to Satisfy Flutter Requirements
  • References

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