Overview

Structural Dynamics in Aeronautical Engineering is a comprehensive introduction to the modern methods of dynamic analysis of aeronautical structures. The text is particularly suitable for undergraduate students. For advanced students, the text provides numerous references on seminal work on structural dynamics that can be used for graduate level research. The text represents carefully developed course materials, beginning with an introductory chapter on matrix algebra and methods for numerical computations, followed by a series of chapters discussing specific aeronautical applications. In this way, the student can be guided from the simple concept of a single-degree-of-freedom structural system to the more complex multiple-degree-of-freedom and continuous systems, including random vibrations, nonlinear systems and aeroelastic phenomena. Among the various examples used in the text, the chapter on aeroelasticity of flight vehicles is particularly noteworthy with its clear presentation of the phenomena and its mathematical formulation for structural and aerodynamic loads.

Full Product Details

Author:   Maher N.Bismarck- Naar
Publisher:   American Institute of Aeronautics & Astronautics
Imprint:   American Institute of Aeronautics & Astronautics
Dimensions:   Width: 15.80cm , Height: 2.10cm , Length: 23.00cm
Weight:   0.649kg
ISBN:  

9781563473234

ISBN 10:   1563473232
Pages:   300
Publication Date:   31 March 1999
Audience:   College/higher education ,  Professional and scholarly ,  Undergraduate ,  Postgraduate, Research & Scholarly
Format:   Hardback
Publisher's Status:   Active
Availability:   Out of stock  
The supplier is temporarily out of stock of this item. It will be ordered for you on backorder and shipped when it becomes available.

Table of Contents

Matrix Algebra and Techniques; Single-Degree-of-Freedom Linear System; Multidegree-of-Freedom Linear Systems; Dynamics of Continuous Elastic Bodies; Nonlinear Systems; Random Vibrations; The Typical Section in Aeroelasticity; Aeroelasticity of Flight Vehicles; Aeroelasticity of Plates and Shells.

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