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E-grāmata: Introduction to Aircraft Structural Analysis

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(Professor Emeritus, Department of Civil Engineering, Leeds University, UK (deceased))
  • Formāts: EPUB+DRM
  • Izdošanas datums: 25-Oct-2013
  • Izdevniecība: Butterworth-Heinemann Ltd
  • Valoda: eng
  • ISBN-13: 9780080982038
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Introduction to Aircraft Structural AnalysisPalielināt
  • Formāts: EPUB+DRM
  • Izdošanas datums: 25-Oct-2013
  • Izdevniecība: Butterworth-Heinemann Ltd
  • Valoda: eng
  • ISBN-13: 9780080982038
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Based on the author's best-selling text, Aircraft Structures for Engineering Students, this brief book covers the basics of structural analysis as applied to aircraft structures Coverage of elasticity, energy methods and virtual work set the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations. Self-contained, this value-priced book is an excellent resource for anyone learning the subject.

  • Based on the author's best-selling text Aircraft Structures for Engineering Students, this introduction covers core concepts in about 200 fewer pages than the original by removing some optional topics like structural vibrations and aeroelasticity
  • Systematic step-by-step procedures in the worked examples
  • Self-contained, with complete derivations for key equations

Papildus informācija

An essential resource for learning aircraft structural analysis, at a value price!
Preface xi
PART A FUNDAMENTALS OF STRUCTURAL ANALYSIS
Section A1 Elasticity
3(2)
Chapter 1 Basic elasticity
5(42)
1.1 Stress
5(2)
1.2 Notation for forces and stresses
7(2)
1.3 Equations of equilibrium
9(2)
1.4 Plane stress
11(1)
1.5 Boundary conditions
11(1)
1.6 Determination of stresses on inclined planes
12(3)
1.7 Principal stresses
15(2)
1.8 Mohr's circle of stress
17(5)
1.9 Strain
22(3)
1.10 Compatibility equations
25(1)
1.11 Plane strain
26(1)
1.12 Determination of strains on inclined planes
27(2)
1.13 Principal strains
29(1)
1.14 Mohr's circle of strain
30(1)
1.15 Stress---strain relationships
30(7)
1.16 Experimental measurement of surface strains
37(10)
References
43(1)
Problems
43(4)
Chapter 2 Two-dimensional problems in elasticity
47(22)
2.1 Two-dimensional problems
47(2)
2.2 Stress functions
49(1)
2.3 Inverse and semi-inverse methods
50(6)
2.4 St. Venant's principle
56(1)
2.5 Displacements
57(1)
2.6 Bending of an end-loaded cantilever
58(11)
Reference
63(1)
Problems
63(6)
Chapter 3 Torsion of solid sections
69(22)
3.1 Prandtl stress function solution
69(12)
3.2 St. Venant warping function solution
81(1)
3.3 The membrane analogy
82(2)
3.4 Torsion of a narrow rectangular strip
84(7)
References
86(1)
Problems
87(2)
Section A2 Virtual work, energy, and matrix methods
89(2)
Chapter 4 Virtual work and energy methods
91(32)
4.1 Work
91(1)
4.2 Principle of virtual work
92(14)
4.3 Applications of the principle of virtual work
106(17)
Reference
117(1)
Problems
118(5)
Chapter 5 Energy methods
123(60)
5.1 Strain energy and complementary energy
123(2)
5.2 Principle of the stationary value of the total complementary energy
125(1)
5.3 Application to deflection problems
126(9)
5.4 Application to the solution of statically indeterminate systems
135(17)
5.5 Unit load method
152(3)
5.6 Flexibility method
155(5)
5.7 Total potential energy
160(1)
5.8 Principle of the stationary value of the total potential energy
161(3)
5.9 Principle of superposition
164(1)
5.10 Reciprocal theorem
164(4)
5.11 Temperature effects
168(15)
References
171(1)
Problems
171(12)
Chapter 6 Matrix methods
183(50)
6.1 Notation
184(1)
6.2 Stiffness matrix for an elastic spring
185(1)
6.3 Stiffness matrix for two elastic springs in line
186(3)
6.4 Matrix analysis of pin-jointed frameworks
189(7)
6.5 Application to statically indeterminate frameworks
196(1)
6.6 Matrix analysis of space frames
196(2)
6.7 Stiffness matrix for a uniform beam
198(7)
6.8 Finite element method for continuum structures
205(28)
References
223(1)
Further reading
223(1)
Problems
223(8)
Section A3 Thin plate theory
231(2)
Chapter 7 Bending of thin plates
233(36)
7.1 Pure bending of thin plates
233(3)
7.2 Plates subjected to bending and twisting
236(4)
7.3 Plates subjected to a distributed transverse load
240(10)
7.4 Combined bending and in-plane loading of a thin rectangular plate
250(4)
7.5 Bending of thin plates having a small initial curvature
254(1)
7.6 Energy method for the bending of thin plates
255(14)
Further reading
263(1)
Problems
263(4)
Section A4 Structural instability
267(2)
Chapter 8 Columns
269(42)
8.1 Euler buckling of columns
269(6)
8.2 Inelastic buckling
275(4)
8.3 Effect of initial imperfections
279(3)
8.4 Stability of beams under transverse and axial loads
282(4)
8.5 Energy method for the calculation of buckling loads in columns
286(3)
8.6 Flexural---torsional buckling of thin-walled columns
289(22)
References
301(1)
Problems
302(9)
Chapter 9 Thin plates
311(34)
9.1 Buckling of thin plates
311(3)
9.2 Inelastic buckling of plates
314(2)
9.3 Experimental determination of the critical load for a flat plate
316(1)
9.4 Local instability
316(1)
9.5 Instability of stiffened panels
317(2)
9.6 Failure stress in plates and stiffened panels
319(3)
9.7 Tension field beams
322(23)
References
338(1)
Problems
338(7)
PART B ANALYSIS OF AIRCRAFT STRUCTURES
Section B1 Principles of stressed skin construction
345(2)
Chapter 10 Materials
347(24)
10.1 Aluminum alloys
347(2)
10.2 Steel
349(1)
10.3 Titanium
350(1)
10.4 Plastics
351(1)
10.5 Glass
351(1)
10.6 Composite materials
351(2)
10.7 Properties of materials
353(18)
Problems
368(3)
Chapter 11 Structural components of aircraft
371(24)
11.1 Loads on structural components
371(2)
11.2 Function of structural components
373(5)
11.3 Fabrication of structural components
378(5)
11.4 Connections
383(12)
Reference
389(1)
Problems
389(4)
Section B2 Airworthiness and airframe loads
393(2)
Chapter 12 Airworthiness
395(6)
12.1 Factors of the safety-flight envelope
395(2)
12.2 Load factor determination
397(4)
Reference
400(1)
Problems
400(1)
Chapter 13 Airframe loads
401(30)
13.1 Aircraft inertia loads
401(6)
13.2 Symmetric maneuver loads
407(5)
13.3 Normal accelerations associated with various types of maneuver
412(4)
13.4 Gust loads
416(15)
References
424(1)
Problems
424(7)
Chapter 14 Fatigue
431(26)
14.1 Safe life and fail-safe structures
431(1)
14.2 Designing against fatigue
432(1)
14.3 Fatigue strength of components
433(6)
14.4 Prediction of aircraft fatigue life
439(6)
14.5 Crack propagation
445(12)
References
452(1)
Further reading
452(1)
Problems
452(3)
Section B3 Bending, shear and torsion of thin-walled beams
455(2)
Chapter 15 Bending of open and closed, thin-walled beams
457(54)
15.1 Symmetrical bending
458(8)
15.2 Unsymmetrical bending
466(7)
15.3 Deflections due to bending
473(15)
15.4 Calculation of section properties
488(9)
15.5 Applicability of bending theory
497(1)
15.6 Temperature effects
497(14)
Reference
501(1)
Problems
501(10)
Chapter 16 Shear of beams
511(32)
16.1 General stress, strain, and displacement relationships for open and single-cell closed section thin-walled beams
511(4)
16.2 Shear of open section beams
515(9)
16.3 Shear of closed section beams
524(19)
Reference
533(1)
Problems
533(10)
Chapter 17 Torsion of beams
543(24)
17.1 Torsion of closed section beams
543(10)
17.2 Torsion of open section beams
553(14)
Problems
559(8)
Chapter 18 Combined open and closed section beams
567(12)
18.1 Bending
567(2)
18.2 Shear
569(3)
18.3 Torsion
572(7)
Problems
577(2)
Chapter 19 Structural idealization
579(26)
19.1 Principle
579(1)
19.2 Idealization of a panel
580(2)
19.3 Effect of idealization on the analysis of open and closed section beams
582(12)
19.4 Deflection of open and closed section beams
594(11)
Problems
597(6)
Section B4 Stress analysis of aircraft components
603(2)
Chapter 20 Wing spars and box beams
605(14)
20.1 Tapered wing spar
605(4)
20.2 Open and closed section beams
609(5)
20.3 Beams having variable stringer areas
614(5)
Problems
617(2)
Chapter 21 Fuselages
619(10)
21.1 Bending
619(2)
21.2 Shear
621(2)
21.3 Torsion
623(2)
21.4 Cut-outs in fuselages
625(4)
Problems
626(3)
Chapter 22 Wings
629(34)
22.1 Three-boom shell
629(1)
22.2 Bending
630(1)
22.3 Torsion
631(5)
22.4 Shear
636(7)
22.5 Shear center
643(1)
22.6 Tapered wings
643(3)
22.7 Deflections
646(1)
22.8 Cut-outs in wings
647(16)
Problems
655(8)
Chapter 23 Fuselage frames and wing ribs
663(12)
23.1 Principles of stiffener/web construction
663(5)
23.2 Fuselage frames
668(1)
23.3 Wing ribs
669(6)
Problems
673(2)
Chapter 24 Laminated composite structures
675(32)
24.1 Elastic constants of a simple lamina
675(6)
24.2 Stress---strain relationships for an orthotropic ply (macro approach)
681(9)
24.3 Thin-walled composite beams
690(17)
References
702(1)
Problems
702(5)
Index 707
T.H.G. Megson was a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he wrote 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.
Biežāk uzdotie jautājumi par e-grāmatām Biežāk uzdotie jautājumi par e-grāmatām
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