Aircraft structures for engineering students

Başlık:

Yazar:

Megson, T. H. G. (Thomas Henry Gordon).

ISBN:

9780750667395

Ek Yazar:

Megson, T. H. G. (Thomas Henry Gordon).

Edition:

4. bs.

Yayım Bilgisi:

Oxford ; Burlington, MA : Butterworth-Heinemann, 2010.

Fiziksel Tanım:

xx, 804 s. : tbl., şkl. ; 25 cm.

Series:

Elsevier aerospace engineering series.

Contents:

pt. I. Fundamentals of structural analysis. Elasticity ; Virtual work, energy and matrix methods ; Thin plate theory ; Structural instability ; Vibration of structures -- pt. II. Analysis of aircraft structures. Principles of stressed skin construction ; Airworthiness and airframe loads ; Bending, shear and torsion of thin-walled beams ; Stress analysis of aircraft components ; Structural and loading discontinuities -- Introduction to aeroelasticity.

Konu Terimleri:

Uçak gövdesi.

Airframes.

Mevcut:*

Library	Materyal Türü	Barkod	Yer Numarası	Durum
Searching... Pamukkale Merkez Kütüphanesi	Kitap	0060250	TL671.6.M36 2010	Searching... Unknown

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Özet

Aircraft Structures for Engineering Students is the leading self contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its fourth edition, the author has revised and updated the text throughout and added new case study and worked example material to make the text even more accessible.

Author Notes

T.H.G. Megson is a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he has written the market leading Butterworth Heinemann textbooks Aircraft Structures for Engineering Students and Introduction to Aircraft Structural Analysis (a briefer derivative of the aircraft structures book), as well as the text/ref hybrid Structural and Stress Analysis.

Part A Fundamentals of Structural Analysis

A I Elasticity

1 Basic elasticity

2 Two-dimensional problems in elasticity

3 Torsion of solid sections

A II Virtual Work, Energy and Matrix Methods

4 Virtual work

5 Energy methods

6 Matrix methods

A III Thin Plate Theory

7 Bending of thin plates

A IV Structural Instability

8 Columns

9 Thin plates

10 Structural Vibration

Part B Analysis of Aircraft Structures

B I Principles of Stressed Skin Construction

11 Materials

12 Structural components of aircraft

B II Airworthiness and Airframe Loads

13 Airworthiness

14 Airframe loads

15 Fatigue

B III Bending, Shear and Torsion of Thin-Walled Beams

16 Bending of open and closed, Thin-Walled Beams

17 Shear of beams

18 Torsion of beams

19 Combined open and closed section beams

20 Structural Idealisation B IV Stress Analysis of Aircraft Components

21 Wing spars and box beams

22 Fuselages

23 Wings

24 Fuselage frames and wing ribs

25 Laminated composite structures BV Structural and Loading Discontinuities

26 Closed section beams

27 Open section beams

B VI

28 Wing problems

Appendix

Case Study: Design of an Aircraft Fuselage

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Author Notes

Table of Contents