MARC details
000 -LEADER |
fixed length control field |
21978cam a2200313 a 4500 |
001 - CONTROL NUMBER |
control field |
16027813 |
003 - CONTROL NUMBER IDENTIFIER |
control field |
BUL |
005 - DATE AND TIME OF LATEST TRANSACTION |
control field |
20210319135853.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
091218s2010 ne a b 001 0 eng |
010 ## - LIBRARY OF CONGRESS CONTROL NUMBER |
LC control number |
2009050354 |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
International Standard Book Number |
9781856179324 (pbk. : alk. paper) |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
International Standard Book Number |
185617932X (pbk. : alk. paper) |
035 ## - SYSTEM CONTROL NUMBER |
System control number |
(OCoLC)ocn490807676 |
040 ## - CATALOGING SOURCE |
Original cataloging agency |
BUL |
Transcribing agency |
BUL |
Modifying agency |
BUL |
-- |
BUL |
-- |
BUL |
-- |
BUL |
-- |
BUL |
100 1# - MAIN ENTRY--PERSONAL NAME |
Personal name |
Megson, T. H. G. |
Fuller form of name |
(Thomas Henry Gordon) |
245 13 - TITLE STATEMENT |
Title |
An introduction to aircraft structural analysis / |
Statement of responsibility, etc. |
T.H.G. Megson. |
250 ## - EDITION STATEMENT |
Edition statement |
4th Ed. |
260 ## - PUBLICATION, DISTRIBUTION, ETC. |
Place of publication, distribution, etc. |
Amsterdam ; |
-- |
Boston : |
Name of publisher, distributor, etc. |
Butterworth-Heinemann/Elsevier, |
Date of publication, distribution, etc. |
c2010. |
300 ## - PHYSICAL DESCRIPTION |
Extent |
vii, 638 p. : |
Other physical details |
ill. ; |
Dimensions |
24 cm. |
500 ## - GENERAL NOTE |
General note |
Contents<br/>Preface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vii<br/>PART A FUNDAMENTALS OF STRUCTURAL ANALYSIS<br/>CHAPTER 1 Basic Elasticity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3<br/>1.1 Stress .................................................................................................. 3<br/>1.2 Notation for Forces and Stresses ................................................................... 5<br/>1.3 Equations of Equilibrium ........................................................................... 7<br/>1.4 Plane Stress ........................................................................................... 9<br/>1.5 Boundary Conditions ................................................................................ 9<br/>1.6 Determination of Stresses on Inclined Planes .................................................... 10<br/>1.7 Principal Stresses .................................................................................... 14<br/>1.8 Mohr’s Circle of Stress .............................................................................. 16<br/>1.9 Strain .................................................................................................. 20<br/>1.10 Compatibility Equations ............................................................................ 24<br/>1.11 Plane Strain ........................................................................................... 25<br/>1.12 Determination of Strains on Inclined Planes...................................................... 25<br/>1.13 Principal Strains ...................................................................................... 27<br/>1.14 Mohr’s Circle of Strain .............................................................................. 28<br/>1.15 Stress–Strain Relationships ......................................................................... 28<br/>1.16 Experimental Measurement of Surface Strains ................................................... 37<br/>Problems .............................................................................................. 41<br/>CHAPTER 2 Two-Dimensional Problems in Elasticity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45<br/>2.1 Two-Dimensional Problems ........................................................................ 45<br/>2.2 Stress Functions ...................................................................................... 47<br/>2.3 Inverse and Semi-Inverse Methods ................................................................ 48<br/>2.4 St. Venant’s Principle ................................................................................ 53<br/>2.5 Displacements ........................................................................................ 54<br/>2.6 Bending of an End-Loaded Cantilever ............................................................ 55<br/>Problems .............................................................................................. 60<br/>CHAPTER 3 Torsion of Solid Sections . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65<br/>3.1 Prandtl Stress Function Solution ................................................................... 65<br/>3.2 St. VenantWarping Function Solution ............................................................ 75<br/>3.3 The Membrane Analogy ............................................................................ 77<br/>3.4 Torsion of a Narrow Rectangular Strip ............................................................ 79<br/>Problems .............................................................................................. 82<br/>CHAPTER 4 Virtual Work and Energy Methods . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85<br/>4.1 Work ................................................................................................... 85<br/>4.2 Principle of VirtualWork ........................................................................... 86<br/>4.3 Applications of the Principle of VirtualWork .................................................... 99<br/>Problems .............................................................................................. 107<br/>CHAPTER 5 Energy Methods . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 111<br/>5.1 Strain Energy and Complementary Energy ....................................................... 111<br/>5.2 The Principle of the Stationary Value of the Total Complementary Energy .................. 113<br/>iii<br/>iv Contents<br/>5.3 Application to Deflection Problems ............................................................... 114<br/>5.4 Application to the Solution of Statically Indeterminate Systems............................... 122<br/>5.5 Unit Load Method ................................................................................... 138<br/>5.6 Flexibility Method ................................................................................... 141<br/>5.7 Total Potential Energy ............................................................................... 147<br/>5.8 The Principle of the Stationary Value of the Total Potential Energy ........................... 148<br/>5.9 Principle of Superposition .......................................................................... 151<br/>5.10 The Reciprocal Theorem............................................................................ 151<br/>5.11 Temperature Effects ................................................................................. 156<br/>Problems .............................................................................................. 158<br/>CHAPTER 6 Matrix Methods. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 169<br/>6.1 Notation ............................................................................................... 170<br/>6.2 Stiffness Matrix for an Elastic Spring ............................................................. 171<br/>6.3 Stiffness Matrix for Two Elastic Springs in Line................................................. 172<br/>6.4 Matrix Analysis of Pin-jointed Frameworks ...................................................... 176<br/>6.5 Application to Statically Indeterminate Frameworks ............................................ 183<br/>6.6 Matrix Analysis of Space Frames .................................................................. 183<br/>6.7 Stiffness Matrix for a Uniform Beam.............................................................. 185<br/>6.8 Finite Element Method for Continuum Structures ............................................... 193<br/>Problems .............................................................................................. 211<br/>CHAPTER 7 Bending of Thin Plates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 219<br/>7.1 Pure Bending of Thin Plates ........................................................................ 219<br/>7.2 Plates Subjected to Bending and Twisting ........................................................ 223<br/>7.3 Plates Subjected to a Distributed Transverse Load............................................... 227<br/>7.4 Combined Bending and In-Plane Loading of a Thin Rectangular Plate ....................... 236<br/>7.5 Bending of Thin Plates Having a Small Initial Curvature ....................................... 240<br/>7.6 Energy Method for the Bending of Thin Plates .................................................. 241<br/>Problems .............................................................................................. 250<br/>CHAPTER 8 Columns . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 253<br/>8.1 Euler Buckling of Columns ......................................................................... 253<br/>8.2 Inelastic Buckling .................................................................................... 259<br/>8.3 Effect of Initial Imperfections ...................................................................... 263<br/>8.4 Stability of Beams under Transverse and Axial Loads .......................................... 266<br/>8.5 Energy Method for the Calculation of Buckling Loads in Columns ........................... 270<br/>8.6 Flexural–Torsional Buckling of Thin-Walled Columns ......................................... 274<br/>Problems .............................................................................................. 287<br/>CHAPTER 9 Thin Plates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 293<br/>9.1 Buckling of Thin Plates ............................................................................. 293<br/>9.2 Inelastic Buckling of Plates ......................................................................... 296<br/>9.3 Experimental Determination of Critical Load for a Flat Plate .................................. 298<br/>9.4 Local Instability ...................................................................................... 299<br/>9.5 Instability of Stiffened Panels ...................................................................... 300<br/>9.6 Failure Stress in Plates and Stiffened Panels...................................................... 302<br/>9.7 Tension Field Beams ................................................................................ 304<br/>Problems .............................................................................................. 320<br/>Contents v<br/>PART B ANALYSIS OF AIRCRAFT STRUCTURES<br/>CHAPTER 10 Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 327<br/>10.1 Aluminum Alloys .................................................................................... 327<br/>10.2 Steel ................................................................................................... 329<br/>10.3 Titanium............................................................................................... 330<br/>10.4 Plastics ................................................................................................ 331<br/>10.5 Glass ................................................................................................... 331<br/>10.6 Composite Materials................................................................................. 331<br/>10.7 Properties of Materials .............................................................................. 333<br/>Problems .............................................................................................. 349<br/>CHAPTER 11 Structural Components of Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 351<br/>11.1 Loads on Structural Components .................................................................. 351<br/>11.2 Function of Structural Components................................................................ 354<br/>11.3 Fabrication of Structural Components ............................................................. 359<br/>11.4 Connections........................................................................................... 363<br/>Problems .............................................................................................. 370<br/>CHAPTER 12 Airworthiness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 373<br/>12.1 Factors of Safety-Flight Envelope ................................................................. 373<br/>12.2 Load Factor Determination ......................................................................... 375<br/>CHAPTER 13 Airframe Loads . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 379<br/>13.1 Aircraft Inertia Loads................................................................................ 379<br/>13.2 Symmetric Maneuver Loads ........................................................................ 386<br/>13.3 Normal Accelerations Associated with Various Types of Maneuver .......................... 391<br/>13.4 Gust Loads ............................................................................................ 393<br/>Problems .............................................................................................. 399<br/>CHAPTER 14 Fatigue . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 403<br/>14.1 Safe Life and Fail-Safe Structures ................................................................. 403<br/>14.2 Designing Against Fatigue .......................................................................... 404<br/>14.3 Fatigue Strength of Components ................................................................... 405<br/>14.4 Prediction of Aircraft Fatigue Life................................................................. 409<br/>14.5 Crack Propagation ................................................................................... 414<br/>Problems .............................................................................................. 420<br/>CHAPTER 15 Bending of Open and Closed, Thin-Walled Beams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 423<br/>15.1 Symmetrical Bending................................................................................ 424<br/>15.2 Unsymmetrical Bending ............................................................................ 433<br/>15.3 Deflections due to Bending ......................................................................... 441<br/>15.4 Calculation of Section Properties .................................................................. 456<br/>15.5 Applicability of Bending Theory................................................................... 466<br/>15.6 Temperature Effects ................................................................................. 466<br/>Problems .............................................................................................. 471<br/>CHAPTER 16 Shear of Beams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 479<br/>16.1 General Stress, Strain, and Displacement Relationships for Open<br/>and Single Cell Closed Section Thin-Walled Beams ............................................ 479<br/>16.2 Shear of Open Section Beams ...................................................................... 483<br/>vi Contents<br/>16.3 Shear of Closed Section Beams .................................................................... 488<br/>Problems .............................................................................................. 496<br/>CHAPTER 17 Torsion of Beams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 503<br/>17.1 Torsion of Closed Section Beams .................................................................. 503<br/>17.2 Torsion of Open Section Beams.................................................................... 514<br/>Problems .............................................................................................. 521<br/>CHAPTER 18 Combined Open and Closed Section Beams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 529<br/>18.1 Bending ............................................................................................... 529<br/>18.2 Shear................................................................................................... 529<br/>18.3 Torsion ................................................................................................ 533<br/>Problems .............................................................................................. 534<br/>CHAPTER 19 Structural Idealization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 537<br/>19.1 Principle............................................................................................... 537<br/>19.2 Idealization of a Panel ............................................................................... 538<br/>19.3 Effect of Idealization on the Analysis of Open and Closed Section Beams................... 541<br/>19.4 Deflection of Open and Closed Section Beams .................................................. 553<br/>Problems .............................................................................................. 556<br/>CHAPTER 20 Wing Spars and Box Beams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 561<br/>20.1 TaperedWing Spar................................................................................... 561<br/>20.2 Open and Closed Section Beams................................................................... 565<br/>20.3 Beams Having Variable Stringer Areas............................................................ 571<br/>Problems .............................................................................................. 574<br/>CHAPTER 21 Fuselages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 577<br/>21.1 Bending ............................................................................................... 577<br/>21.2 Shear................................................................................................... 578<br/>21.3 Torsion ................................................................................................ 581<br/>21.4 Cutouts in Fuselages ................................................................................. 584<br/>Problems .............................................................................................. 585<br/>CHAPTER 22 Wings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 587<br/>22.1 Three-Boom Shell ................................................................................... 587<br/>22.2 Bending ............................................................................................... 588<br/>22.3 Torsion ................................................................................................ 590<br/>22.4 Shear................................................................................................... 594<br/>22.5 Shear Center .......................................................................................... 599<br/>22.6 TaperedWings........................................................................................ 600<br/>22.7 Deflections ............................................................................................ 603<br/>22.8 Cutouts inWings ..................................................................................... 605<br/>Problems .............................................................................................. 613<br/>CHAPTER 23 Fuselage Frames and Wing Ribs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 619<br/>23.1 Principles of Stiffener/Web Construction ......................................................... 619<br/>23.2 Fuselage Frames ..................................................................................... 625<br/>23.3 Wing Ribs ............................................................................................. 626<br/>Problems .............................................................................................. 630<br/>Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 633 |
504 ## - BIBLIOGRAPHY, ETC. NOTE |
Bibliography, etc. note |
Includes bibliographical references and index. |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Airframes. |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Structural analysis (Engineering) |
700 1# - ADDED ENTRY--PERSONAL NAME |
Personal name |
Megson, T. H. G. |
Fuller form of name |
(Thomas Henry Gordon). |
Title of a work |
Aircraft structures for engineering students. |
856 ## - ELECTRONIC LOCATION AND ACCESS |
Materials specified |
Full text E-book in PDF |
Uniform Resource Identifier |
<a href="https://www.pdfdrive.com/aircraft-structures-by-megson-d9155224.html">https://www.pdfdrive.com/aircraft-structures-by-megson-d9155224.html</a> |
Link text |
https://www.pdfdrive.com/aircraft-structures-by-megson-d9155224.html |
906 ## - LOCAL DATA ELEMENT F, LDF (RLIN) |
a |
7 |
b |
cbc |
c |
orignew |
d |
1 |
e |
ecip |
f |
20 |
g |
y-gencatlg |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Source of classification or shelving scheme |
Dewey Decimal Classification |
Koha item type |
Book Open Access |
Edition |
4th Ed. |
Item part |
1 |