Aircraft structures for engineering students:
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Amsterdam [u.a.]
Elsevier
2013
|
Ausgabe: | 5. ed. |
Schriftenreihe: | Elsevier aerospace engineering series
|
Schlagworte: | |
Online-Zugang: | Inhaltsverzeichnis |
Beschreibung: | Includes bibliographical references and index |
Beschreibung: | XV, 859 S. graph. Darst. 24 cm |
ISBN: | 9780080969053 0080969054 |
Internformat
MARC
LEADER | 00000nam a2200000 c 4500 | ||
---|---|---|---|
001 | BV039883692 | ||
003 | DE-604 | ||
005 | 20220105 | ||
007 | t | ||
008 | 120213s2013 d||| |||| 00||| eng d | ||
015 | |a GBB1C0836 |2 dnb | ||
020 | |a 9780080969053 |9 978-0-08-096905-3 | ||
020 | |a 0080969054 |9 0-08-096905-4 | ||
035 | |a (OCoLC)780116446 | ||
035 | |a (DE-599)BVBBV039883692 | ||
040 | |a DE-604 |b ger |e rakwb | ||
041 | 0 | |a eng | |
049 | |a DE-703 |a DE-1050 |a DE-20 |a DE-573 |a DE-861 | ||
084 | |a ZO 7250 |0 (DE-625)157842: |2 rvk | ||
100 | 1 | |a Megson, Thomas H. G. |e Verfasser |4 aut | |
245 | 1 | 0 | |a Aircraft structures for engineering students |c T.H.G. Megson |
250 | |a 5. ed. | ||
264 | 1 | |a Amsterdam [u.a.] |b Elsevier |c 2013 | |
300 | |a XV, 859 S. |b graph. Darst. |c 24 cm | ||
336 | |b txt |2 rdacontent | ||
337 | |b n |2 rdamedia | ||
338 | |b nc |2 rdacarrier | ||
490 | 0 | |a Elsevier aerospace engineering series | |
500 | |a Includes bibliographical references and index | ||
650 | 4 | |a Airframes | |
650 | 0 | 7 | |a Luftfahrzeug |0 (DE-588)4168246-4 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Zelle |0 (DE-588)4067537-3 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Flugzeug |0 (DE-588)4017672-1 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Elastizität |0 (DE-588)4014159-7 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Flugzeugbau |0 (DE-588)4154782-2 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Strukturmechanik |0 (DE-588)4126904-4 |2 gnd |9 rswk-swf |
689 | 0 | 0 | |a Flugzeugbau |0 (DE-588)4154782-2 |D s |
689 | 0 | 1 | |a Strukturmechanik |0 (DE-588)4126904-4 |D s |
689 | 0 | |5 DE-604 | |
689 | 1 | 0 | |a Flugzeug |0 (DE-588)4017672-1 |D s |
689 | 1 | 1 | |a Strukturmechanik |0 (DE-588)4126904-4 |D s |
689 | 1 | |8 1\p |5 DE-604 | |
689 | 2 | 0 | |a Zelle |0 (DE-588)4067537-3 |D s |
689 | 2 | |8 2\p |5 DE-604 | |
689 | 3 | 0 | |a Elastizität |0 (DE-588)4014159-7 |D s |
689 | 3 | |8 3\p |5 DE-604 | |
689 | 4 | 0 | |a Luftfahrzeug |0 (DE-588)4168246-4 |D s |
689 | 4 | |8 4\p |5 DE-604 | |
856 | 4 | 2 | |m Digitalisierung UB Bayreuth |q application/pdf |u http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=024742861&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |3 Inhaltsverzeichnis |
999 | |a oai:aleph.bib-bvb.de:BVB01-024742861 | ||
883 | 1 | |8 1\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk | |
883 | 1 | |8 2\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk | |
883 | 1 | |8 3\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk | |
883 | 1 | |8 4\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk |
Datensatz im Suchindex
_version_ | 1804148829421830144 |
---|---|
adam_text | Contents
Preface
.................................................................................................................................................xv
PART A FUNDAMENTALS OF STRUCTURAL ANALYSIS
________________
Section A1 Elasticity
...........................................................................3
CHAPTER
1
Basic elasticity
...............................................................................................5
1.1
Stress
...........................................................................................................................5
1.2
Notation for forces and stresses
.................................................................................7
1.3
Equations of equilibrium
............................................................................................9
1.4
Plane stress
...............................................................................................................11
1.5
Boundary conditions
.................................................................................................11
1.6
Determination of stresses on inclined planes
..........................................................12
1.7
Principal stresses
......................................................................................................15
1.8
Mohr s circle of stress
.............................................................................................17
1.9
Strain
.........................................................................................................................22
1.10
Compatibility equations
...........................................................................................25
1.11
Plane strain
...............................................................................................................26
1.12
Determination of strains on inclined planes
............................................................27
1.13
Principal strains
........................................................................................................29
1.14
Mohr s circle of strain
.............................................................................................30
1.15
Stress-strain relationships
........................................................................................30
1.16
Experimental measurement of surface strains
.........................................................37
References
.................................................................................................................43
Problems
...................................................................................................................43
CHAPTER
2
Two-dimensional problems in elasticity
.........................................................47
2.1
Two-dimensional problems
......................................................................................47
2.2
Stress functions
.........................................................................................................49
2.3
Inverse and semi-inverse methods
...........................................................................50
2.4
St. Venant s principle
...............................................................................................56
2.5
Displacements
...........................................................................................................57
2.6
Bending of an end-loaded cantilever
.......................................................................58
Reference
..................................................................................................................63
Problems
...................................................................................................................63
CHAPTER
3
Torsion of solid sections
...............................................................................69
3.1
Prandtl stress function solution
................................................................................69
3.2
St.
Venant
warping function solution
......................................................................81
vii
viii Contents
3.3
The membrane analogy
............................................................................................82
3.4
Torsion of a narrow rectangular strip
......................................................................84
References
.................................................................................................................86
Problems
...................................................................................................................87
Section A2 Virtual work, energy, and matrix methods
.........................89
CHAPTER
4
Virtual work and energy methods
..................................................................91
4.1
Work
.........................................................................................................................91
4.2
Principle of virtual work
..........................................................................................92
4.3
Applications of the principle of virtual work
.......................................................106
Reference
................................................................................................................117
Problems
.................................................................................................................118
CHAPTER
5
Energy methods
..........................................................................................123
5.1
Strain energy and complementary energy
.............................................................123
5.2
Principle of the stationary value of the total complementary
energy
.....................................................................................................................125
5.3
Application to deflection problems
.......................................................................126
5.4
Application to the solution of statically indeterminate systems
...........................135
5.5
Unit load method
....................................................................................................152
5.6
Flexibility method
..................................................................................................155
5.7
Total potential energy
............................................................................................160
5.8
Principle of the stationary value of the total potential energy
.............................161
5.9
Principle of superposition
......................................................................................164
5.10
Reciprocal theorem
................................................................................................164
5.11
Temperature effects
................................................................................................168
References
...............................................................................................................171
Problems
.................................................................................................................171
CHAPTER
6
Matrix methods
...........................................................................................183
6.1
Notation
..................................................................................................................184
6.2
Stiffness matrix for an elastic spring
.....................................................................185
6.3
Stiffness matrix for two elastic springs in line
.....................................................186
6.4
Matrix analysis of pin-jointed frameworks
...........................................................189
6.5
Application to statically indeterminate frameworks
.............................................196
6.6
Matrix analysis of space frames
............................................................................196
6.7
Stiffness matrix for a uniform beam
.....................................................................198
6.8
Finite element method for continuum structures
..................................................205
References
...............................................................................................................223
Further reading
.......................................................................................................223
Problems
.................................................................................................................223
Contents ix
Section
A3
Thin plate theory
............................................................231
CHAPTER
7
Bending of thin plates
.................................................................................233
7.1
Pure bending of thin plates
....................................................................................233
7.2
Plates subjected to bending and twisting
..............................................................236
7.3
Plates subjected to a distributed transverse load
..................................................240
7.4
Combined bending and in-plane loading of a thin rectangular plate
...................250
7.5
Bending of thin plates having a small initial curvature
.......................................254
7.6
Energy method for the bending of thin plates
......................................................255
Further reading
.......................................................................................................263
Problems
.................................................................................................................263
Section
A4
Structural instability
.......................................................267
CHAPTER
8
Columns
.....................................................................................................269
8.1
Euler
buckling of columns
.....................................................................................269
8.2
Inelastic buckling
...................................................................................................275
8.3
Effect of initial imperfections
................................................................................279
8.4
Stability of beams under transverse and axial loads
............................................282
8.5
Energy method for the calculation of buckling loads in columns
.......................286
8.6
Flexural-torsional buckling of thin-walled columns
............................................289
References
...............................................................................................................301
Problems
.................................................................................................................302
CHAPTER
9
Thin plates
.................................................................................................311
9.1
Buckling of thin plates
...........................................................................................311
9.2
Inelastic buckling of plates
....................................................................................314
9.3
Experimental determination of the critical load for a flat plate
..........................316
9.4
Local instability
......................................................................................................316
9.5
Instability of stiffened panels
................................................................................317
9.6
Failure stress in plates and stiffened panels
..........................................................319
9.7
Tension field beams
...............................................................................................322
References
...............................................................................................................338
Problems
.................................................................................................................338
Section A5 Vibration of structures
....................................................343
CHAPTER
10
Structural vibration
.....................................................................................345
10.1
Oscillation of mass-spring systems
.......................................................................345
10.2
Oscillation of beams
...............................................................................................354
10.3
Approximate methods for determining natural frequencies
.................................359
Problems
.................................................................................................................362
Contents
PART
В
ANALYSIS OF AIRCRAFT STRUCTURES
______________________
Section B1 Principles of stressed skin
construction
......................................................................................369
CHAPTER
11
Materials
...................................................................................................371
11.1
Aluminum alloys
....................................................................................................371
11.2
Steel
........................................................................................................................373
11.3
Titanium
..................................................................................................................374
11.4
Plastics
....................................................................................................................375
11.5
Glass
.......................................................................................................................375
11.6
Composite materials
...............................................................................................375
11.7
Properties of materials
...........................................................................................377
Problems
.................................................................................................................392
CHAPTER
12
Structural components of aircraft
................................................................395
12.1
Loads on structural components
............................................................................395
12.2
Function of structural components
........................................................................397
12.3
Fabrication of structural components
....................................................................402
12.4
Connections
............................................................................................................407
Reference
................................................................................................................413
Problems
.................................................................................................................413
Section B2 Airworthiness and airframe loads
....................................417
CHAPTER
13
Airworthiness
.............................................................................................419
13.1
Factors of the safety-flight envelope
.....................................................................419
13.2
Load factor determination
......................................................................................421
Reference
................................................................................................................424
CHAPTER
14
Airframe loads
............................................................................................425
14.1
Aircraft inertia loads
..............................................................................................425
14.2
Symmetric maneuver loads
....................................................................................431
14.3
Normal accelerations associated with various types
of maneuver
............................................................................................................436
14.4
Gust loads
...............................................................................................................440
References
...............................................................................................................448
Problems
.................................................................................................................448
CHAPTER
15
Fatigue
.......................................................................................................455
15.1
Safe life and fail-safe structures
............................................................................455
15.2
Designing against fatigue
.......................................................................................456
15.3
Fatigue strength of components
.............................................................................457
15.4
Prediction of aircraft fatigue life
...........................................................................463
Contents xi
15.5
Crack propagation
..................................................................................................469
References
...............................................................................................................476
Further reading
.......................................................................................................476
Problems
.................................................................................................................476
Section B3 Bending, shear and torsion of thin-walled
beams
...........................................................................479
CHAPTER
16
Bending of open and closed, thin-walled beams
...........................................481
16.1
Symmetrical bending
..............................................................................................482
16.2
Unsymmetrical bending
.........................................................................................490
16.3
Deflections due to bending
....................................................................................497
16.4
Calculation of section properties
...........................................................................512
16.5
Applicability of bending theory
.............................................................................521
16.6
Temperature effects
................................................................................................521
Reference
................................................................................................................525
Problems
.................................................................................................................525
CHAPTER
17
Shear of beams
..........................................................................................535
17.1
General stress, strain, and displacement relationships for open and
single-cell closed section thin-walled beams
........................................................535
17.2
Shear of open section beams
.................................................................................539
17.3
Shear of closed section beams
...............................................................................548
Reference
................................................................................................................557
Problems
.................................................................................................................557
CHAPTER
18
Torsion of beams
........................................................................................567
18.1
Torsion of closed section beams
...........................................................................567
18.2
Torsion of open section beams
..............................................................................577
Problems
.................................................................................................................583
CHAPTER
19
Combined open and closed section beams
...................................................591
19.1
Bending
...................................................................................................................591
19.2
Shear
.......................................................................................................................593
19.3
Torsion
....................................................................................................................596
Problems
.................................................................................................................601
CHAPTER
20
Structural idealization
................................................................................603
20.1
Principle
..................................................................................................................603
20.2
Idealization of a panel
............................................................................................604
20.3
Effect of idealization on the analysis of open and closed section
beams
......................................................................................................................606
20.4
Deflection of open and closed section beams
.......................................................618
Problems
.................................................................................................................621
xii Contents
Section
В4
Stress
analysis of aircraft components
............................627
CHAPTER
21
Wing spars and box beams
.........................................................................629
21.1
Tapered wing spar
..................................................................................................629
21.2
Open and closed section beams
.............................................................................633
21.3
Beams having variable stringer areas
....................................................................638
Problems
.................................................................................................................641
CHAPTER
22
Fuselages
...................................................................................................643
22.1
Bending
...................................................................................................................643
22.2
Shear
.......................................................................................................................645
22.3
Torsion
....................................................................................................................647
22.4
Cut-outs in fuselages
..............................................................................................649
Problems
.................................................................................................................650
CHAPTER
23
Wings
........................................................................................................653
23.1
Three-boom shell
....................................................................................................653
23.2
Bending
...................................................................................................................654
23.3
Torsion
....................................................................................................................655
23.4
Shear
.......................................................................................................................660
23.5
Shear center
............................................................................................................667
23.6
Tapered wings
........................................................................................................667
23.7
Deflections
..............................................................................................................670
23.8
Cut-outs in wings
...................................................................................................671
Problems
.................................................................................................................679
CHAPTER
24
Fuselage frames and wing ribs
....................................................................687
24.1
Principles of stiffener/web construction
................................................................687
24.2
Fuselage frames
......................................................................................................692
24.3
Wing ribs
................................................................................................................693
Problems
.................................................................................................................697
CHAPTER
25
Laminated composite structures
..................................................................699
25.1
Elastic constants of a simple lamina
.....................................................................699
25.2
Stress-strain relationships for an orthotropic ply (macro approach)
...................705
25.3
Thin-walled composite beams
...............................................................................714
References
...............................................................................................................726
Problems
.................................................................................................................726
Section B5 Structural and loading discontinuities
.............................731
CHAPTER
26
Closed section beams
.................................................................................733
26.1
General aspects
.......................................................................................................733
Contents xiii
26.2
Shear stress distribution at a built-in end of a closed section beam
....................734
26.3
Thin-walled rectangular section beam subjected to torsion
.................................740
26.4
Shear lag
.................................................................................................................748
Reference
................................................................................................................765
Problems
.................................................................................................................765
CHAPTER
27
Open section beams
....................................................................................773
27.1
I-section beam subjected to torsion
.......................................................................773
27.2
Torsion of an arbitrary section beam
....................................................................775
27.3
Distributed torque loading
.....................................................................................785
27.4
Extension of the theory to allow for general systems of loading
........................787
27.5
Moment couple (bimoment)
..................................................................................790
References
...............................................................................................................793
Problems
.................................................................................................................793
Section B6 Introduction to aeroelasticity
..........................................799
CHAPTER
28
Wing problems
...........................................................................................801
28.1
Types of problem
...................................................................................................801
28.2
Load distribution and divergence
..........................................................................802
28.3
Control effectiveness and reversal
.........................................................................808
28.4
Introduction to flutter
.........................................................................................814
References
...............................................................................................................821
Problems
.................................................................................................................821
Appendix: Design of a rear fuselage
....................................................................................825
Index
..................................................................................................................................853
|
any_adam_object | 1 |
author | Megson, Thomas H. G. |
author_facet | Megson, Thomas H. G. |
author_role | aut |
author_sort | Megson, Thomas H. G. |
author_variant | t h g m thg thgm |
building | Verbundindex |
bvnumber | BV039883692 |
classification_rvk | ZO 7250 |
ctrlnum | (OCoLC)780116446 (DE-599)BVBBV039883692 |
discipline | Verkehr / Transport |
edition | 5. ed. |
format | Book |
fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>02507nam a2200613 c 4500</leader><controlfield tag="001">BV039883692</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20220105 </controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">120213s2013 d||| |||| 00||| eng d</controlfield><datafield tag="015" ind1=" " ind2=" "><subfield code="a">GBB1C0836</subfield><subfield code="2">dnb</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9780080969053</subfield><subfield code="9">978-0-08-096905-3</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">0080969054</subfield><subfield code="9">0-08-096905-4</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)780116446</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV039883692</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-703</subfield><subfield code="a">DE-1050</subfield><subfield code="a">DE-20</subfield><subfield code="a">DE-573</subfield><subfield code="a">DE-861</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">ZO 7250</subfield><subfield code="0">(DE-625)157842:</subfield><subfield code="2">rvk</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Megson, Thomas H. G.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Aircraft structures for engineering students</subfield><subfield code="c">T.H.G. Megson</subfield></datafield><datafield tag="250" ind1=" " ind2=" "><subfield code="a">5. ed.</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Amsterdam [u.a.]</subfield><subfield code="b">Elsevier</subfield><subfield code="c">2013</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">XV, 859 S.</subfield><subfield code="b">graph. Darst.</subfield><subfield code="c">24 cm</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="490" ind1="0" ind2=" "><subfield code="a">Elsevier aerospace engineering series</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">Includes bibliographical references and index</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Airframes</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Luftfahrzeug</subfield><subfield code="0">(DE-588)4168246-4</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Zelle</subfield><subfield code="0">(DE-588)4067537-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Flugzeug</subfield><subfield code="0">(DE-588)4017672-1</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Elastizität</subfield><subfield code="0">(DE-588)4014159-7</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Flugzeugbau</subfield><subfield code="0">(DE-588)4154782-2</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Strukturmechanik</subfield><subfield code="0">(DE-588)4126904-4</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Flugzeugbau</subfield><subfield code="0">(DE-588)4154782-2</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="1"><subfield code="a">Strukturmechanik</subfield><subfield code="0">(DE-588)4126904-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="1" ind2="0"><subfield code="a">Flugzeug</subfield><subfield code="0">(DE-588)4017672-1</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2="1"><subfield code="a">Strukturmechanik</subfield><subfield code="0">(DE-588)4126904-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2=" "><subfield code="8">1\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="2" ind2="0"><subfield code="a">Zelle</subfield><subfield code="0">(DE-588)4067537-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="2" ind2=" "><subfield code="8">2\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="3" ind2="0"><subfield code="a">Elastizität</subfield><subfield code="0">(DE-588)4014159-7</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="3" ind2=" "><subfield code="8">3\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="4" ind2="0"><subfield code="a">Luftfahrzeug</subfield><subfield code="0">(DE-588)4168246-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="4" ind2=" "><subfield code="8">4\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="856" ind1="4" ind2="2"><subfield code="m">Digitalisierung UB Bayreuth</subfield><subfield code="q">application/pdf</subfield><subfield code="u">http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=024742861&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA</subfield><subfield code="3">Inhaltsverzeichnis</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-024742861</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">1\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">2\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">3\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">4\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield></record></collection> |
id | DE-604.BV039883692 |
illustrated | Illustrated |
indexdate | 2024-07-10T00:13:21Z |
institution | BVB |
isbn | 9780080969053 0080969054 |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-024742861 |
oclc_num | 780116446 |
open_access_boolean | |
owner | DE-703 DE-1050 DE-20 DE-573 DE-861 |
owner_facet | DE-703 DE-1050 DE-20 DE-573 DE-861 |
physical | XV, 859 S. graph. Darst. 24 cm |
publishDate | 2013 |
publishDateSearch | 2013 |
publishDateSort | 2013 |
publisher | Elsevier |
record_format | marc |
series2 | Elsevier aerospace engineering series |
spelling | Megson, Thomas H. G. Verfasser aut Aircraft structures for engineering students T.H.G. Megson 5. ed. Amsterdam [u.a.] Elsevier 2013 XV, 859 S. graph. Darst. 24 cm txt rdacontent n rdamedia nc rdacarrier Elsevier aerospace engineering series Includes bibliographical references and index Airframes Luftfahrzeug (DE-588)4168246-4 gnd rswk-swf Zelle (DE-588)4067537-3 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Elastizität (DE-588)4014159-7 gnd rswk-swf Flugzeugbau (DE-588)4154782-2 gnd rswk-swf Strukturmechanik (DE-588)4126904-4 gnd rswk-swf Flugzeugbau (DE-588)4154782-2 s Strukturmechanik (DE-588)4126904-4 s DE-604 Flugzeug (DE-588)4017672-1 s 1\p DE-604 Zelle (DE-588)4067537-3 s 2\p DE-604 Elastizität (DE-588)4014159-7 s 3\p DE-604 Luftfahrzeug (DE-588)4168246-4 s 4\p DE-604 Digitalisierung UB Bayreuth application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=024742861&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 2\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 3\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 4\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
spellingShingle | Megson, Thomas H. G. Aircraft structures for engineering students Airframes Luftfahrzeug (DE-588)4168246-4 gnd Zelle (DE-588)4067537-3 gnd Flugzeug (DE-588)4017672-1 gnd Elastizität (DE-588)4014159-7 gnd Flugzeugbau (DE-588)4154782-2 gnd Strukturmechanik (DE-588)4126904-4 gnd |
subject_GND | (DE-588)4168246-4 (DE-588)4067537-3 (DE-588)4017672-1 (DE-588)4014159-7 (DE-588)4154782-2 (DE-588)4126904-4 |
title | Aircraft structures for engineering students |
title_auth | Aircraft structures for engineering students |
title_exact_search | Aircraft structures for engineering students |
title_full | Aircraft structures for engineering students T.H.G. Megson |
title_fullStr | Aircraft structures for engineering students T.H.G. Megson |
title_full_unstemmed | Aircraft structures for engineering students T.H.G. Megson |
title_short | Aircraft structures for engineering students |
title_sort | aircraft structures for engineering students |
topic | Airframes Luftfahrzeug (DE-588)4168246-4 gnd Zelle (DE-588)4067537-3 gnd Flugzeug (DE-588)4017672-1 gnd Elastizität (DE-588)4014159-7 gnd Flugzeugbau (DE-588)4154782-2 gnd Strukturmechanik (DE-588)4126904-4 gnd |
topic_facet | Airframes Luftfahrzeug Zelle Flugzeug Elastizität Flugzeugbau Strukturmechanik |
url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=024742861&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
work_keys_str_mv | AT megsonthomashg aircraftstructuresforengineeringstudents |