MARC details
| 000 -LEADER |
|---|
| fixed length control field |
02942cam a22004457i 4500 |
| 001 - CONTROL NUMBER |
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| control field |
20503785 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20241004072425.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
180519s2017 ne a 001 0 eng d |
| 010 ## - LIBRARY OF CONGRESS CONTROL NUMBER |
|---|
| LC control number |
2016461697 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
9780081009147 |
| Qualifying information |
(paperback) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
0081009143 |
| Qualifying information |
(paperback) |
| 035 ## - SYSTEM CONTROL NUMBER |
|---|
| System control number |
(OCoLC)ocn954224012 |
| 040 ## - CATALOGING SOURCE |
|---|
| Original cataloging agency |
YDXCP |
| Language of cataloging |
eng |
| Transcribing agency |
YDXCP |
| Description conventions |
rda |
| Modifying agency |
OCLCQ |
| -- |
SHS |
| -- |
LTSCA |
| -- |
OCLCF |
| -- |
ZWZ |
| -- |
LIP |
| -- |
VLB |
| -- |
DLC |
| 042 ## - AUTHENTICATION CODE |
|---|
| Authentication code |
lccopycat |
| 050 00 - LIBRARY OF CONGRESS CALL NUMBER |
|---|
| Classification number |
TL671.6 MEG |
| Item number |
.M36 2017 |
| 082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
629.1/3431 |
| Edition number |
23 |
| 100 1# - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Megson, T. H. G. |
| Fuller form of name |
(Thomas Henry Gordon), |
| Relator term |
author. |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Aircraft structures for engineering students / |
| Statement of responsibility, etc. |
T.H.G. Megson. |
| 250 ## - EDITION STATEMENT |
|---|
| Edition statement |
Sixth edition. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE |
|---|
| Place of production, publication, distribution, manufacture |
Amsterdam ; |
| -- |
Boston : |
| Name of producer, publisher, distributor, manufacturer |
Butterworth-Heinemann is an imprint of Elsevier, |
| Date of production, publication, distribution, manufacture, or copyright notice |
[2017] |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
xvii, 891 pages : |
| Other physical details |
illustrations ; |
| Dimensions |
24 cm. |
| 336 ## - CONTENT TYPE |
|---|
| Content type term |
text |
| Content type code |
txt |
| Source |
rdacontent |
| 337 ## - MEDIA TYPE |
|---|
| Media type term |
unmediated |
| Media type code |
n |
| Source |
rdamedia |
| 338 ## - CARRIER TYPE |
|---|
| Carrier type term |
volume |
| Carrier type code |
nc |
| Source |
rdacarrier |
| 490 1# - SERIES STATEMENT |
|---|
| Series statement |
Elsevier aerospace engineering series |
| 500 ## - GENERAL NOTE |
|---|
| General note |
Includes index and illustrations |
| 505 0# - FORMATTED CONTENTS NOTE |
|---|
| Formatted contents note |
Part A. Fundamentals of structural analysis. Section A1. Elasticity. Basic elasticity -- Two-dimensional problems in elasticity -- Torsion of solid sections -- Section A2. Virtual work, energy, and matrix methods. Virtual work and energy methods -- Energy methods -- Matrix methods -- Section A3. Thin plate theory. Bending of thin plates -- Section A4. Structural instability. Columns -- Thin plates -- Section A5. Vibration of structures. Structural vibration -- -- Part B. Analysis of aircraft structures. Section B1. Principles of stressed skin construction. Materials -- Structural components of aircraft -- Section B2. Airworthiness and airframe loads. Airworthiness -- Airframe loads -- Fatigue -- Section B3. Bending, shear and torsion of thin-walled beams. Bending of open and closed, thin-walled beams -- Shear of beams -- Torsion of beams -- Combined open and closed section beams -- Structural idealization -- Section B4. Stress analysis of aircraft components. Wing spars and box beams -- Fuselages -- Wings -- Fuselage frames and wing ribs -- Laminated composite structures -- Section B5. Structural and loading discontinuities. Closed section beams -- Open section beams -- Section B6. Introduction to aeroelasticity. Wing problems -- Appendix : Design of a rear fuselage. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Airframes |
| Form subdivision |
Textbooks. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Structural analysis (Engineering) |
| Form subdivision |
Textbooks. |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Airframes. |
| Source of heading or term |
fast |
| Authority record control number or standard number |
(OCoLC)fst00802910 |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Structural analysis (Engineering) |
| Source of heading or term |
fast |
| Authority record control number or standard number |
(OCoLC)fst01135602 |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Avions |
| General subdivision |
Conception et construction. |
| Source of heading or term |
ram |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Avions |
| General subdivision |
Vibrations. |
| Source of heading or term |
ram |
| 655 #7 - INDEX TERM--GENRE/FORM |
|---|
| Genre/form data or focus term |
Textbooks. |
| Source of term |
fast |
| Authority record control number or standard number |
(OCoLC)fst01423863 |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE |
|---|
| Uniform title |
Elsevier aerospace engineering series. |
| 906 ## - LOCAL DATA ELEMENT F, LDF (RLIN) |
|---|
| a |
7 |
| b |
cbc |
| c |
copycat |
| d |
2 |
| e |
ncip |
| f |
20 |
| g |
y-gencatlg |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Source of classification or shelving scheme |
Library of Congress Classification |
| Koha item type |
Books |