Aircraft structures for engineering students:
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| Format: | Book |
| Language: | English |
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Amsterdam
Elsevier, Butterworth-Heinemann
[2022]
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| Edition: | Seventh edition |
| Series: | Aerospace engineering
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| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Item Description: | Forthcoming publication |
| Physical Description: | xv, 944 Seiten Illustrationen, Diagramme |
| ISBN: | 9780128228685 0128228687 |
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| 100 | 1 | |a Megson, T. H. G. |d 1934- |e Verfasser |0 (DE-588)1055777008 |4 aut | |
| 245 | 1 | 0 | |a Aircraft structures for engineering students |c T.H.G. Megson |
| 250 | |a Seventh edition | ||
| 264 | 1 | |a Amsterdam |b Elsevier, Butterworth-Heinemann |c [2022] | |
| 264 | 4 | |c © 2022 | |
| 300 | |a xv, 944 Seiten |b Illustrationen, Diagramme | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 0 | |a Aerospace engineering | |
| 500 | |a Forthcoming publication | ||
| 650 | 4 | |a Airframes | |
| 650 | 4 | |a Structural analysis (Engineering) | |
| 650 | 4 | |a Airframes -- Textbooks | |
| 650 | 4 | |a Structural analysis (Engineering) -- Textbooks | |
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| 776 | 0 | 8 | |i Erscheint auch als |n Online-Ausgabe |z 978-0-32390211-3 |
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Contents
Preface to the Seventh Edition of Aircraft Structures XV
PART A FUNDAMENTALS OF STRUCTURAL ANALYSIS
Section Al Elasticity ccsssseecseessennesseensenenseenseeeseeesecereceeectrsnenes O
CHAPTER 1 Basic elasticity uuncssesseneeesnenenenennnennsennnenenenennunnenrnennnentnenensnennsennnennnensnnnennnene 5
1 1 Stress eessssscessesssenseseceaseecsseeseerecesseeseeesenessaes tee 5
1 2 Notation for forces and Stresses cscsessscsessssssessesesesssseseasentsessenesnsesesreeseenseenesees 7
1 3 Equations of equilibrium
1 4 Plane stress eee
1 5 Boundary conditions
1 6 Determination of stresses on inclined planes ueseneesesesenennsensntsnusenensonenrennnntnnnen
1 7 Principal stresses n0eessnenssasensesesessnsnnensenenntnenenntentenensontnnnnnrossnsassnssenorrasennne
1 8 Mohr’s circle of stress enenssensennsenensnnnennnenerentnnnsnnursnsenensasnennnsnsenansessessnonnenenennara
1 9 Strain eesssssssensssesnsennensentntsentnrsensnnennenenensnsnsnsenentnnsententntososeen nes nnssnats
1 10 Compatibility equations anareeseesensensessnsesensensntennennernennensnnenrensenter ran
1 11 Plane strain ucsennesensessseneersansnsensnnennnsssn innen
1 12 Determination of strains on inclined planes
1 13 Principal strains enessesseeeneneennnenteennnn
1 14 Mohr’s circle of strain
1 15 Stress-strain relationships
1 16 Experimental measurement of surface strains eeereseennessensenessensenssensenssonteneene 42
Reference cc csescscsscssssscscasessrssecesesseresenenescescscsenuarsesseeseesnenssesensanensesaaneaeosonsasueseanereanaes
Further reading
Problems ccccccsssscessecccessssecsececeeneneesesseeenesesteestsesuseseseaesenensacoseneeeressesteneseneatenentarers
CHAPTER 2 Two-dimensional problems in elasticity we 53
2 1 Two-dimensional problems
2 2 Stress functionS asnesssnsnneneneneenenenennnnnnnnsenentenenennnrorssnrtnensnnn
2 3 Inverse and semi-inverse methods
2 4 St Venant’s principle
2 5 Displacements
2 6 Bending of an end-loaded cantilever 64
Reference ccccceccececsesssssscsescsessesesesesecerseacsenseaneuenessstensanseaseueaesesseatsocorseeuereseseseensanengats 70
Problems
CHAPTER 3 Torsion of solid sections 75
3 1 Prandtl stress function solution 75
3 2 St Venant warping function solution
3 3 The membrane analogy nnmmmmmmmemenmenmemernesseenennmnerssennunnnennnnnnnnng 30
3 4 Torsion of a narrow rectangular StTIPoovvsseenssenseeneeenseeessetnsettsntastttstinttinsies , 9
References unsnsensnsenensenensenseroenstosontnsssensnsossssnsnssnnntnnnsssnssnnennnensnnnnnn
Peer 94
Problems nennnunneennnnneeenennsernnnseneernnenneereennnenentettsrnnnnnentttsnennnnetssnnnnnnnnnnnnn 94
Section A2 Virtual work, energy, and matrix methods „een 97
CHAPTER 4 Virtual work and energy methods
41 Work eeeeseensssssenesonnennennnnnonsennnnennnenns
5 2 Principle of the stationary value of the total complementary energy
5 3 Application to deflection problem 0 ssssssssssssessecsessessssaresatececssessessseessccssseces
5 4 Application to the solution of statically indeterminate systems
5 5 Unit load method sscsscssccsssssnsssssssssecsessessessnssusssssecsessesaeereseesecsessarsessseens
5 6 Flexibility method csssssssssssssssssesessessessscesssscsevsussesscsesarsvcaesessesavseseareesees
5 7 Total potential energy ssccsscssssssssessessessssessvssscessssssavoussecacsesatsresesersetsessees
5 8 Principle of the stationary value of the total potential energy
5 9 Principle of superposition seccssssessssssessssssesssessesaesssessessssssssesstessesseesssesscesseees
5 10 Reciprocal theorem c csccssssssssessecsssecsssssssscsssssessecssseavsassscasececrecessecurarsaveneeecaveeess
5 11 Temperature effects ecsecssscsssssecseessessessssssesssecaecssessecssessssaeeansesscssessecssessseeseeess
References cesses essessssesseescenscessecseaeasesesessesscosesssussssssusscsssanescansacesesessecsesseeseeeeets
Farther reading
Problems scscssessssesseceeseseeessesesseseaeenesensssesessssesesessesesecsesessescaueseessesseaseeaseneseeses
CHAPTER 6 Matrix methods sssscsssssssecsssccssssvescessessesssececseesaeessseceusesneecseessneeenneeeeses
GoT Notation on ec ssescsescescessessessesosssssssssesssssssscsssnssssssceacsocesesseeaseessaees
6 2 Stiffness matrix for an elastic spring
6 3 Stiffness matrix for two elastic springs in line
6 4 Matrix analysis of pin-jointed frameworkS ccceseseeseees
6 5 Application to statically indeterminate frameworks neenenennneteeen 207
6 6 Matrix analysis of space frames cuseneensnenssnsensusnennennontnsnnnnnannanensenssernnnenennt
6 7 Stiffness matrix for a uniform beam uenenensnensennnanansannonnnnnnennnennnnnnsnsanennenennrantntnt
References cccccsscscceesescosecesscsesesssesecesscessesenssseececssesorecseceescsensecsesucsneesenseeeeeseeseee®
Further reading
Problems ccccccccsssssossstsssccecsscecescessscessescesssecsaeseresscsscsecsececnucensuacecacesecaasenseesseeeees
Section A3 Thin plate theory
CHAPTER 7 Bending of thin plates cc scesssscscssccocsssessessscecssssssssesesessececesccosec 245
7 1 Pure bending of thin plates c ccccscssssessssssessscssssesssssssssssseneecassesesensssesecessnsseseeeesese 245
7 2 Plates subjected to bending and twisting 248
7 3 Plates subjected to a distributed transverse load ana wee 252
7 4 Combined bending and in-plane loading of a thin rectangular plate 263
7 5 Bending of thin plates having a small initial curvature anne 267
7 6 Energy method for the bending of thin plates cc csssssccsssssesescececccuessseeeesseses 267
Further reading
PrODIOMs ccssccsessssssessecsseensecueeceeensssuesusessssusssseasecsscenscnssesecsnessucansesnesaesrarsseceneenerese
Section A4 Structural instability cccccsccccssscssrrssessscsscrsseeerees 281
CHAPTER 8 Columns seesesecseccosssssssseesseessesssresssesssssseesssesssessseeraeessusceseeraueraseensestaceee 283
8 1 Euler buckling of ColUmins scessssssscesseessssecseesersccsssseesteseenecsucsuesersavaneseesesessens 283
8 2 Inelastic Duckling 0 sssssssssssesssssssssssssesssessecseessesosssssssueccecescssresseaseecscenectasenees 291
8 3 Effect of initial imperfections cccccsssssessssssssssssssssccsessessesecsectecteresersesseeseaees 296
8 4 Stability of beams under transverse and axial loads c csccccessecesseceseeseseesececseens 300
8 5 Energy method for the calculation of buckling loads in columns csscssee 304
8 6 Flexural-torsional buckling of thin-walled columns «unse «+ 308
References Svesceseesecscegeusnesstentesaesaesnecssseesstesceass u 320
Problems ecccccseccssssessssscecsesscsescscesessssencsenscesacacsevcceccssssssectcsauceseseacavenctvavaeesssvseaeas 320
CHAPTER 9 = Thin plates ccccsssscsscsccsscssscsssssssseesesesneecsecerseceseecsesersecaeansaseceesarareeteces 331
9 1 Buckling of thin plates
9 2 Inelastic buckling of plates cscssssssssesssssssssesssesseesssssessstessestenees ve 335
9 3 Experimental determination of the critical load for a flat plate scssseeese 337
9 4 Local instability eesssssssessssessescscsssececsssssessesesssesscsssessesessseseeecaeesssensessneseeceess 337
9 5 Instability of stiffened panels ccessscsssscecsessesessssessssesatsssessssscsseseesesasseesessesees 338
9 6 Failure stress in plates and stiffened panels ssecssssssssssssseessseseeeseessseeseenses 340
9 7 Tension field Deas cccscsssssesscssessesesessesessesesescseesesescsscessesussssesesesssecoesesseseseses 347
References ccecessseescescsssesesssensnsscarsesesescsesescaesesessseacaeseacarseacseseseaessesssaresoseranssacares 362
Problems ueesessssssssssnansnsorenennenenennenanenennnnsnnnnenenenennensononsnnsornssenesnsnsnssssnsensssnenen 363
Section AS Vibration of structures uneeeenerenennnnnnannnennnannnnnnnenenuunnnune GOD
CHAPTER 10 Structural vibration an nenensnnnnnananstsennnnonnanssnnane 371
10 1 Oscillation of mass-spring systems enenensscsesnsenennsnnnennennnnnnennnenensnennnronnnnsnnnnnnone 371
10 2 Oscillation of beams 381
10 3 Approximate methods for determining natural frequencies ccesseeceeesees 386
PART B ANALYSIS OF AIRCRAFT STRUCTURES
Section B1 Principles of stressed skin construction
sateatesesaeseeeces seve 395
CHAPTER 11 Materials „un
LIT luminary ce itcteteessssreessssseetssenstaseeesasteiatsiaeee 397
UMURUM AllOyS nennen 397
11 2 Steel rrvsvovereeneneennceneceessnscenegnauansnsceteetsvssnsseeeesisssseeettnssirstitasitieeseec 399
11 3 THANE eereerenennnnnninnttnnttinnnnnitttiinninec 400
11 4 Polymers
11 5 Glass
Section B2 Airworthiness and airframe CT
CHAPTER 13 Airworthiness cccssssssssscccsssssssesssssssssssssesusssoseceesececceseeeseseeeeccecececcccces
13 1 Factors of Safety: Flight envelope ccscccscscscsssssssesecssssssssesesseesescussuececeseceasenses
13 2 Load factor determination u cssscccsssssssssssssssssssessssssssssssssessececesessasssssssssssssesseensene
13 3 Airworthiness: Spacecraft cccccccssssssscssccccsssssssssscecsssssssescssssssssssssssessessssesesseseseee
RePEreNnCe seescsesseecssesssessecsnensessssesssecsuccensesaressucessscssusesavecsusesssuccsasecssavecsssuceeecasees
Problems sccecssecssssessssssessscssccosssucsruesacesscsaversessucsseccuscsusessvecsucceacesucerneceenseensesess
14 3 Normal accelerations associated with various types of maneuver
14 4 Gust Loads c ccccssssssesssssesessssssssucsusssecsessecsecssesstssnecsessuccnecnuecussaecscssnecasceacceeeessness#
14 5 Design loads: Spacecraft -sscsscsssssssssssssssesscssceossessssasensecarssececssnsssceesseersesenesee?
References cccsccsssseseeseseeeessssesecescseeceeecrstscucencsssssssssscssneacsosssascacsusseessersceseossentees
Problems cscsscscscecetscceessseeesesecssscsnsceccccoesenssssseneseecsecsscsssceuscesecsncassaqsseceeeneesentene?
CHAPTER 15, Fatigue s:csscsscsscessssssssensssees ee
15 1 Safe life and fail-safe structures ccenecceceeseencnnneennennennnnnnnnennunannnsnannannnnennnnananeenene
15 2 Designing against fatigue nesnsenenensensnssossnsessesssssnsensenennenen
15 3 Fatigue strength of components 487
15 4 Prediction of aircraft fatigue life
nenne 493
15 5 Crack propagation 499
References unenensenseeeessensunsennnsnneenenneeennennnnnn 506
Further reading nesnensnnnnnnnnnnn 506
PrODICMS sccscsessssssecscsssssesessssussnesesessasstasasestisssastsecoseteccceesccsss 507
Section B3
CHAPTER 16
CHAPTER 17
CHAPTER 18
CHAPTER 19
CHAPTER 20
Bending, shear, and torsion of thin-walled beams 509
Bending of open and closed thin-walled DeAMS s sssscssssesseseseeecoeeeeecoseecs 511
Symmetrical bending 512
Unsymmetrical bending csecccccessessseseeeee 521
Deflections due to bending wees 529
Calculation of section properties 549
Applicability of bending theory 559
Temperature effects 559
Reference un seoneenereeeeaeeneees 563
Problems ceessssesessessesseseeseenss se seesneneeneesasseaesenentenens 563
Shear of beams c00 573
General stress, strain, and displacement relationships for open and
single-cell closed section thin-walled beams 573
Shear of open section beams 577
Shear of closed section beams 586
Reference uuneesessesenessennenennannenn eeaseneatscaesenesaees 595
Problems ni ssssonneenacarsensenastseseasensoeseacscsenerorcuanatacaeateueusencacacacenees 595
Torsion of beams 605
Torsion of closed section beams 605
Torsion of open section beams 0 615
Problems Sernensssntarsnnene 621
Combined open and closed section beams 629
Bending 629
Shear 631
Torsion 634
Problems 639
Structural idealization 641
Principle 641
Idealization of a panel 642
Effect of idealization on the analysis of open and closed section beams 646
Deflection of open and closed section beaMS c cccccccscecsssscececarsesesecsesecseeseece 659
Problems 662
Section B4 Stress analysis of aircraft and spacecraft components 669
sreeeseneusenensestsnesenecaeseraneaearscuauseuseetsatssaseaeceseersesess 671
21 1 Tapered wing spar ssscssossssssessssssssssseessssssssnsessssesssasesssusecaseessasscssesessssuecessesescesses 671
21 2 Open and closed section beams nnensensssssennsensssnssnnsenuennnsonssensennesmnennnonnnennnnannnnn, 675
21 3 Beams having variable stringer areas scsesscesseessecsesotssesssenssersesterersttesssseceses 680
PrODLOMS ssscscsssssscesescsessecnessssesesesssesssesearacecseseacscesuesssescseasavscseatacesenssarsasanesces 685
CHAPTER 22 Fuselages sesessenseeneeucuceescesteeneusssatsesesuereuevarsesecaeass 689
22 1 Bending uensesessesssessensenssnsensensensensnnnenrensennensenennnontnnsantnnsnnnunnetensonsenennennennnannnunnnne 689
22 2 SHEA escesssesssssesesesessoesesssseseseacscaustsnscecasseaustsavacsestatsseacasseuscssssesesearaverecsarssensensens 691
22 3 Torsion ccscssssssssesssssssscescsesessesssenesessseseseussessaesessstensaesesessesesssecccscssssaececararasseases 693
22 4 Pressurized fuselages os ecssscssssscseesssecnssssesesseseenseesesensseesesssessssesessessesssnsanans 695
22 5 Cut-outs in fuselages secscssececssesssessesesessnessessesssessssesssssssssssessesseatacenseacsaensaes 702
Reference ccececssssessesessssessoeseesescseessessacsecessceeessseesecseseeseeesenssassesessesecacsesesessasass 707
Problems c scssssssssseseseesescscusesescesesesaessscsscsussesesaesesessesnsnessenssesausesacseeaeeasasecsessenees 707
CHAPTER 23 Wings cscsccsssssseesserssoessceorscasaecrareesesueesesersesuerseareuseeseesenceseeceeeeees 711
23 1 Three-boom shell ccccsssssssssssssssssssscsssessssssscnesssnssesesesenseeseuseseeesestenearsesesseeseaees 711
23 2 Bending scccscssscssssssssssesesesessseeesesesestseeessestsseeceesesssesestaceeesesssneneseneassqseeeseesseerseees 712
23 3 Torsion ccccccssssssscseseesessesescsnsssasscsecsesssssnsssseesestenesssueceseeeesaeaesnenesesseaneneesetanenearsces 714
23 4 Shear cccscssesssssssscncssesessncsseeesessssssessseccesessenesseneaesceacaeseeauseesssscauscseeaesecseansneneassees 718
23 5 Shear Center cscscsscsssssssscessesseeescsessesessssessacsacsessesenesecaesessesacsesssreneensaescenensaceaeeees 725
23 6 Tapered wings ccsscssssssssccsesersesesesesensesssessecnssesenesesensceceqeeseosoeesesseseeasensceceeeseses 725
23 7 Deflections
23 8 Cut-outs in WINgS uncnensscsnsenssensnsnensnennnenennnnnenessensnenensnsennnnsssennnenessnennnnnennnesssantanens 729
Problems ueoesesceneseonennnensnssnenensunsnsnnnennsssassnnnensnssnnsessnonnansnnansnnnonnnonsennansanntennen 737
CHAPTER 24 Fuselage frames and Wing ribS cccccscscsccssscccccecccsecenssersessvarscesecsegesereres 745
24 1 Principles of stiffener/web construction cccsssssssssessssssenensceseessesentenseteeesesees 745
24 2 Fuselage frames
24 3 Wing ribs eucsnsnsussnsnnenonsnnonsnnsossnssnnennenensunuenssnensnensnssnsosnsonnensnsensornsnansensnsernssses
Problems suserseesersnssessunonnonennsnsnnunnssonsnnensnnnnsunsensnnnssnnnsnnennennssnnnnnnnssnennssestsseren
CHAPTER 25 Spacecraft
25 1 Natural frequencies uuensrssnsusesesnscensenenenenensnenenunensnensnronsnnsnsensnsnenenronnensnssnnneennn 757
25 2 Axial Stress ceenesssnessensnnnensansenennnnenensnnnnnesonsensnnenenenssnsnennnnsnannnnennonsenennensnesnserstanserone 758
25 3 Stability u au 759
Reference sus0senesosnneenesnssonsossnennnnnsnssnsssnentensususntansnssnsuannsnnssnsnensssssnorsnssnsssntenen 761
Problems s0srssesassanssnnssennussnnsnsnssssantsnnenonnnnennussnsansessnensennnesensennenonensersnseasttsent 761
CHAPTER 26 Laminated composite structures 763
26 1 Elastic constants of a simple lamina nenecesssanessnnssennanenononannnnnnnenenanannannenenenenrennen 763
26 2 Stress-strain relationships for an orthotropic ply (macro approach) + 769
26 3 Laminates nessesenesnssssnennnesnnennnsnnenennennsnsnensnntunsssunsntnsnnenenenssenenansnnsnsessenesnsnenesene 718
26 4 Thin-walled composite beams
un u deanensacacaeaesesseceeeeearars 795
References ccccccccscsscsssssssecsssessccessnesnseseneccaceneeneserseesececsessccaassecassasseeaeeuasanasevasenss 808
Problems ccccsccsscssscscscsssesecceseeseeencsceneenscesscesseadengeaeensnatssesaressecsesanssesereensasanesnsanes 808
Section B5 Structural and loading discontinuities ccssssceseee 815
CHAPTER 27 Closed section beams ccsssssssccssssscscssesesescnseersesseeeesneecenerersnseseneneuseseses 817
27 1 General aspects oessennneeenennntreensnenn 817
27 2 Shear stress distribution at a built-in end of a closed section beam 818
27 3 Thin-walled rectangular section beam subjected to torsion
27 4 Shear lag
Reference
Problems
CHAPTER 28 Open section beams
28 1 I-Section beam subjected t0 tOTSION «neresenseneennenensnernsenensnnensnennntnsnnessentessnsteneseenn
28 2 Torsion of an arbitrary section beam
28 3 Distributed torque loading eneneneeenennenennenen
28 4 Extension of the theory to allow for general systems of loading eessansnrernensnsstanen 873
28 5 Moment couple (bimoment)
References
Problems
Section B6 Introduction to aeroelasticity uennsuennonnennennennennernnnnnne 885
CHAPTER 29 Wing problems cee u
29 1 Types of problem csesssssssssssesssneecseenesssstsssssnceanecssesasessnseanaceeneenesssonessnerensatens
29 2 Load distribution and divergence
29 3 Control effectiveness and reversal
29 4 Introduction to “flutter” „ne
References
Problems c scccccccecsececeeressssersseesserscescesesseecsenseseseeveesneseseesesansacernecsecaesesecseaenetersneaeaes
Appendix: Design of a rear fuselage 911
Index u 939 |
| adam_txt |
Contents
Preface to the Seventh Edition of Aircraft Structures XV
PART A FUNDAMENTALS OF STRUCTURAL ANALYSIS
Section Al Elasticity ccsssseecseessennesseensenenseenseeeseeesecereceeectrsnenes O
CHAPTER 1 Basic elasticity uuncssesseneeesnenenenennnennsennnenenenennunnenrnennnentnenensnennsennnennnensnnnennnene 5
1 1 Stress eessssscessesssenseseceaseecsseeseerecesseeseeesenessaes tee 5
1 2 Notation for forces and Stresses cscsessscsessssssessesesesssseseasentsessenesnsesesreeseenseenesees 7
1 3 Equations of equilibrium
1 4 Plane stress eee
1 5 Boundary conditions
1 6 Determination of stresses on inclined planes ueseneesesesenennsensntsnusenensonenrennnntnnnen
1 7 Principal stresses n0eessnenssasensesesessnsnnensenenntnenenntentenensontnnnnnrossnsassnssenorrasennne
1 8 Mohr’s circle of stress enenssensennsenensnnnennnenerentnnnsnnursnsenensasnennnsnsenansessessnonnenenennara
1 9 Strain eesssssssensssesnsennensentntsentnrsensnnennenenensnsnsnsenentnnsententntososeen nes nnssnats
1 10 Compatibility equations anareeseesensensessnsesensensntennennernennensnnenrensenter ran
1 11 Plane strain ucsennesensessseneersansnsensnnennnsssn innen
1 12 Determination of strains on inclined planes
1 13 Principal strains enessesseeeneneennnenteennnn
1 14 Mohr’s circle of strain
1 15 Stress-strain relationships
1 16 Experimental measurement of surface strains eeereseennessensenessensenssensenssonteneene 42
Reference cc csescscsscssssscscasessrssecesesseresenenescescscsenuarsesseeseesnenssesensanensesaaneaeosonsasueseanereanaes
Further reading
Problems ccccccsssscessecccessssecsececeeneneesesseeenesesteestsesuseseseaesenensacoseneeeressesteneseneatenentarers
CHAPTER 2 Two-dimensional problems in elasticity we 53
2 1 Two-dimensional problems
2 2 Stress functionS asnesssnsnneneneneenenenennnnnnnnsenentenenennnrorssnrtnensnnn
2 3 Inverse and semi-inverse methods
2 4 St Venant’s principle
2 5 Displacements
2 6 Bending of an end-loaded cantilever 64
Reference ccccceccececsesssssscsescsessesesesesecerseacsenseaneuenessstensanseaseueaesesseatsocorseeuereseseseensanengats 70
Problems
CHAPTER 3 Torsion of solid sections 75
3 1 Prandtl stress function solution 75
3 2 St Venant warping function solution
3 3 The membrane analogy nnmmmmmmmemenmenmemernesseenennmnerssennunnnennnnnnnnng 30
3 4 Torsion of a narrow rectangular StTIPoovvsseenssenseeneeenseeessetnsettsntastttstinttinsies , 9
References unsnsensnsenensenensenseroenstosontnsssensnsossssnsnssnnntnnnsssnssnnennnensnnnnnn
Peer 94
Problems nennnunneennnnneeenennsernnnseneernnenneereennnenentettsrnnnnnentttsnennnnetssnnnnnnnnnnnnn 94
Section A2 Virtual work, energy, and matrix methods „een 97
CHAPTER 4 Virtual work and energy methods
41 Work eeeeseensssssenesonnennennnnnonsennnnennnenns
5 2 Principle of the stationary value of the total complementary energy
5 3 Application to deflection problem 0 ssssssssssssessecsessessssaresatececssessessseessccssseces
5 4 Application to the solution of statically indeterminate systems
5 5 Unit load method sscsscssccsssssnsssssssssecsessessessnssusssssecsessesaeereseesecsessarsessseens
5 6 Flexibility method csssssssssssssssssesessessessscesssscsevsussesscsesarsvcaesessesavseseareesees
5 7 Total potential energy ssccsscssssssssessessessssessvssscessssssavoussecacsesatsresesersetsessees
5 8 Principle of the stationary value of the total potential energy
5 9 Principle of superposition seccssssessssssessssssesssessesaesssessessssssssesstessesseesssesscesseees
5 10 Reciprocal theorem c csccssssssssessecsssecsssssssscsssssessecssseavsassscasececrecessecurarsaveneeecaveeess
5 11 Temperature effects ecsecssscsssssecseessessessssssesssecaecssessecssessssaeeansesscssessecssessseeseeess
References cesses essessssesseescenscessecseaeasesesessesscosesssussssssusscsssanescansacesesessecsesseeseeeeets
Farther reading
Problems scscssessssesseceeseseeessesesseseaeenesensssesessssesesessesesecsesessescaueseessesseaseeaseneseeses
CHAPTER 6 Matrix methods sssscsssssssecsssccssssvescessessesssececseesaeessseceusesneecseessneeenneeeeses
GoT Notation on ec ssescsescescessessessesosssssssssesssssssscsssnssssssceacsocesesseeaseessaees
6 2 Stiffness matrix for an elastic spring
6 3 Stiffness matrix for two elastic springs in line
6 4 Matrix analysis of pin-jointed frameworkS ccceseseeseees
6 5 Application to statically indeterminate frameworks neenenennneteeen 207
6 6 Matrix analysis of space frames cuseneensnenssnsensusnennennontnsnnnnnannanensenssernnnenennt
6 7 Stiffness matrix for a uniform beam uenenensnensennnanansannonnnnnnennnennnnnnsnsanennenennrantntnt
References cccccsscscceesescosecesscsesesssesecesscessesenssseececssesorecseceescsensecsesucsneesenseeeeeseeseee®
Further reading
Problems ccccccccsssssossstsssccecsscecescessscessescesssecsaeseresscsscsecsececnucensuacecacesecaasenseesseeeees
Section A3 Thin plate theory
CHAPTER 7 Bending of thin plates cc scesssscscssccocsssessessscecssssssssesesessececesccosec 245
7 1 Pure bending of thin plates c ccccscssssessssssessscssssesssssssssssseneecassesesensssesecessnsseseeeesese 245
7 2 Plates subjected to bending and twisting 248
7 3 Plates subjected to a distributed transverse load ana wee 252
7 4 Combined bending and in-plane loading of a thin rectangular plate 263
7 5 Bending of thin plates having a small initial curvature anne 267
7 6 Energy method for the bending of thin plates cc csssssccsssssesescececccuessseeeesseses 267
Further reading
PrODIOMs ccssccsessssssessecsseensecueeceeensssuesusessssusssseasecsscenscnssesecsnessucansesnesaesrarsseceneenerese
Section A4 Structural instability cccccsccccssscssrrssessscsscrsseeerees 281
CHAPTER 8 Columns seesesecseccosssssssseesseessesssresssesssssseesssesssessseeraeessusceseeraueraseensestaceee 283
8 1 Euler buckling of ColUmins scessssssscesseessssecseesersccsssseesteseenecsucsuesersavaneseesesessens 283
8 2 Inelastic Duckling 0 sssssssssssesssssssssssssesssessecseessesosssssssueccecescssresseaseecscenectasenees 291
8 3 Effect of initial imperfections cccccsssssessssssssssssssssccsessessesecsectecteresersesseeseaees 296
8 4 Stability of beams under transverse and axial loads c csccccessecesseceseeseseesececseens 300
8 5 Energy method for the calculation of buckling loads in columns csscssee 304
8 6 Flexural-torsional buckling of thin-walled columns «unse «+ 308
References Svesceseesecscegeusnesstentesaesaesnecssseesstesceass u 320
Problems ecccccseccssssessssscecsesscsescscesessssencsenscesacacsevcceccssssssectcsauceseseacavenctvavaeesssvseaeas 320
CHAPTER 9 = Thin plates ccccsssscsscsccsscssscsssssssseesesesneecsecerseceseecsesersecaeansaseceesarareeteces 331
9 1 Buckling of thin plates
9 2 Inelastic buckling of plates cscssssssssesssssssssesssesseesssssessstessestenees ve 335
9 3 Experimental determination of the critical load for a flat plate scssseeese 337
9 4 Local instability eesssssssessssessescscsssececsssssessesesssesscsssessesessseseeecaeesssensessneseeceess 337
9 5 Instability of stiffened panels ccessscsssscecsessesessssessssesatsssessssscsseseesesasseesessesees 338
9 6 Failure stress in plates and stiffened panels ssecssssssssssssseessseseeeseessseeseenses 340
9 7 Tension field Deas cccscsssssesscssessesesessesessesesescseesesescsscessesussssesesesssecoesesseseseses 347
References ccecessseescescsssesesssensnsscarsesesescsesescaesesessseacaeseacarseacseseseaessesssaresoseranssacares 362
Problems ueesessssssssssnansnsorenennenenennenanenennnnsnnnnenenenennensononsnnsornssenesnsnsnssssnsensssnenen 363
Section AS Vibration of structures uneeeenerenennnnnnannnennnannnnnnnenenuunnnune GOD
CHAPTER 10 Structural vibration an nenensnnnnnananstsennnnonnanssnnane 371
10 1 Oscillation of mass-spring systems enenensscsesnsenennsnnnennennnnnnennnenensnennnronnnnsnnnnnnone 371
10 2 Oscillation of beams 381
10 3 Approximate methods for determining natural frequencies ccesseeceeesees 386
PART B ANALYSIS OF AIRCRAFT STRUCTURES
Section B1 Principles of stressed skin construction
sateatesesaeseeeces seve 395
CHAPTER 11 Materials „un
LIT luminary ce itcteteessssreessssseetssenstaseeesasteiatsiaeee 397
UMURUM AllOyS nennen 397
11 2 Steel rrvsvovereeneneennceneceessnscenegnauansnsceteetsvssnsseeeesisssseeettnssirstitasitieeseec 399
11 3 THANE eereerenennnnnninnttnnttinnnnnitttiinninec 400
11 4 Polymers
11 5 Glass
Section B2 Airworthiness and airframe CT
CHAPTER 13 Airworthiness cccssssssssscccsssssssesssssssssssssesusssoseceesececceseeeseseeeeccecececcccces
13 1 Factors of Safety: Flight envelope ccscccscscscsssssssesecssssssssesesseesescussuececeseceasenses
13 2 Load factor determination u cssscccsssssssssssssssssssessssssssssssssessececesessasssssssssssssesseensene
13 3 Airworthiness: Spacecraft cccccccssssssscssccccsssssssssscecsssssssescssssssssssssssessessssesesseseseee
RePEreNnCe seescsesseecssesssessecsnensessssesssecsuccensesaressucessscssusesavecsusesssuccsasecssavecsssuceeecasees
Problems sccecssecssssessssssessscssccosssucsruesacesscsaversessucsseccuscsusessvecsucceacesucerneceenseensesess
14 3 Normal accelerations associated with various types of maneuver
14 4 Gust Loads c ccccssssssesssssesessssssssucsusssecsessecsecssesstssnecsessuccnecnuecussaecscssnecasceacceeeessness#
14 5 Design loads: Spacecraft -sscsscsssssssssssssssesscssceossessssasensecarssececssnsssceesseersesenesee?
References cccsccsssseseeseseeeessssesecescseeceeecrstscucencsssssssssscssneacsosssascacsusseessersceseossentees
Problems cscsscscscecetscceessseeesesecssscsnsceccccoesenssssseneseecsecsscsssceuscesecsncassaqsseceeeneesentene?
CHAPTER 15, Fatigue s:csscsscsscessssssssensssees ee
15 1 Safe life and fail-safe structures ccenecceceeseencnnneennennennnnnnnnennunannnsnannannnnennnnananeenene
15 2 Designing against fatigue nesnsenenensensnssossnsessesssssnsensenennenen
15 3 Fatigue strength of components 487
15 4 Prediction of aircraft fatigue life
nenne 493
15 5 Crack propagation 499
References unenensenseeeessensunsennnsnneenenneeennennnnnn 506
Further reading nesnensnnnnnnnnnnn 506
PrODICMS sccscsessssssecscsssssesessssussnesesessasstasasestisssastsecoseteccceesccsss 507
Section B3
CHAPTER 16
CHAPTER 17
CHAPTER 18
CHAPTER 19
CHAPTER 20
Bending, shear, and torsion of thin-walled beams 509
Bending of open and closed thin-walled DeAMS s sssscssssesseseseeecoeeeeecoseecs 511
Symmetrical bending 512
Unsymmetrical bending csecccccessessseseeeee 521
Deflections due to bending wees 529
Calculation of section properties 549
Applicability of bending theory 559
Temperature effects 559
Reference un seoneenereeeeaeeneees 563
Problems ceessssesessessesseseeseenss se seesneneeneesasseaesenentenens 563
Shear of beams c00 573
General stress, strain, and displacement relationships for open and
single-cell closed section thin-walled beams 573
Shear of open section beams 577
Shear of closed section beams 586
Reference uuneesessesenessennenennannenn eeaseneatscaesenesaees 595
Problems ni ssssonneenacarsensenastseseasensoeseacscsenerorcuanatacaeateueusencacacacenees 595
Torsion of beams 605
Torsion of closed section beams 605
Torsion of open section beams 0 615
Problems Sernensssntarsnnene 621
Combined open and closed section beams 629
Bending 629
Shear 631
Torsion 634
Problems 639
Structural idealization 641
Principle 641
Idealization of a panel 642
Effect of idealization on the analysis of open and closed section beams 646
Deflection of open and closed section beaMS c cccccccscecsssscececarsesesecsesecseeseece 659
Problems 662
Section B4 Stress analysis of aircraft and spacecraft components 669
sreeeseneusenensestsnesenecaeseraneaearscuauseuseetsatssaseaeceseersesess 671
21 1 Tapered wing spar ssscssossssssessssssssssseessssssssnsessssesssasesssusecaseessasscssesessssuecessesescesses 671
21 2 Open and closed section beams nnensensssssennsensssnssnnsenuennnsonssensennesmnennnonnnennnnannnnn, 675
21 3 Beams having variable stringer areas scsesscesseessecsesotssesssenssersesterersttesssseceses 680
PrODLOMS ssscscsssssscesescsessecnessssesesesssesssesearacecseseacscesuesssescseasavscseatacesenssarsasanesces 685
CHAPTER 22 Fuselages sesessenseeneeucuceescesteeneusssatsesesuereuevarsesecaeass 689
22 1 Bending uensesessesssessensenssnsensensensensnnnenrensennensenennnontnnsantnnsnnnunnetensonsenennennennnannnunnnne 689
22 2 SHEA escesssesssssesesesessoesesssseseseacscaustsnscecasseaustsavacsestatsseacasseuscssssesesearaverecsarssensensens 691
22 3 Torsion ccscssssssssesssssssscescsesessesssenesessseseseussessaesessstensaesesessesesssecccscssssaececararasseases 693
22 4 Pressurized fuselages os ecssscssssscseesssecnssssesesseseenseesesensseesesssessssesessessesssnsanans 695
22 5 Cut-outs in fuselages secscssececssesssessesesessnessessesssessssesssssssssssessesseatacenseacsaensaes 702
Reference ccececssssessesessssessoeseesescseessessacsecessceeessseesecseseeseeesenssassesessesecacsesesessasass 707
Problems c scssssssssseseseesescscusesescesesesaessscsscsussesesaesesessesnsnessenssesausesacseeaeeasasecsessenees 707
CHAPTER 23 Wings cscsccsssssseesserssoessceorscasaecrareesesueesesersesuerseareuseeseesenceseeceeeeees 711
23 1 Three-boom shell ccccsssssssssssssssssssscsssessssssscnesssnssesesesenseeseuseseeesestenearsesesseeseaees 711
23 2 Bending scccscssscssssssssssesesesessseeesesesestseeessestsseeceesesssesestaceeesesssneneseneassqseeeseesseerseees 712
23 3 Torsion ccccccssssssscseseesessesescsnsssasscsecsesssssnsssseesestenesssueceseeeesaeaesnenesesseaneneesetanenearsces 714
23 4 Shear cccscssesssssssscncssesessncsseeesessssssessseccesessenesseneaesceacaeseeauseesssscauscseeaesecseansneneassees 718
23 5 Shear Center cscscsscsssssssscessesseeescsessesessssessacsacsessesenesecaesessesacsesssreneensaescenensaceaeeees 725
23 6 Tapered wings ccsscssssssssccsesersesesesesensesssessecnssesenesesensceceqeeseosoeesesseseeasensceceeeseses 725
23 7 Deflections
23 8 Cut-outs in WINgS uncnensscsnsenssensnsnensnennnenennnnnenessensnenensnsennnnsssennnenessnennnnnennnesssantanens 729
Problems ueoesesceneseonennnensnssnenensunsnsnnnennsssassnnnensnssnnsessnonnansnnansnnnonnnonsennansanntennen 737
CHAPTER 24 Fuselage frames and Wing ribS cccccscscsccssscccccecccsecenssersessvarscesecsegesereres 745
24 1 Principles of stiffener/web construction cccsssssssssessssssenensceseessesentenseteeesesees 745
24 2 Fuselage frames
24 3 Wing ribs eucsnsnsussnsnnenonsnnonsnnsossnssnnennenensunuenssnensnensnssnsosnsonnensnsensornsnansensnsernssses
Problems suserseesersnssessunonnonennsnsnnunnssonsnnensnnnnsunsensnnnssnnnsnnennennssnnnnnnnssnennssestsseren
CHAPTER 25 Spacecraft
25 1 Natural frequencies uuensrssnsusesesnscensenenenenensnenenunensnensnronsnnsnsensnsnenenronnensnssnnneennn 757
25 2 Axial Stress ceenesssnessensnnnensansenennnnenensnnnnnesonsensnnenenenssnsnennnnsnannnnennonsenennensnesnserstanserone 758
25 3 Stability u au 759
Reference sus0senesosnneenesnssonsossnennnnnsnssnsssnentensususntansnssnsuannsnnssnsnensssssnorsnssnsssntenen 761
Problems s0srssesassanssnnssennussnnsnsnssssantsnnenonnnnennussnsansessnensennnesensennenonensersnseasttsent 761
CHAPTER 26 Laminated composite structures 763
26 1 Elastic constants of a simple lamina nenecesssanessnnssennanenononannnnnnnenenanannannenenenenrennen 763
26 2 Stress-strain relationships for an orthotropic ply (macro approach) + 769
26 3 Laminates nessesenesnssssnennnesnnennnsnnenennennsnsnensnntunsssunsntnsnnenenenssenenansnnsnsessenesnsnenesene 718
26 4 Thin-walled composite beams
un u deanensacacaeaesesseceeeeearars 795
References ccccccccscsscsssssssecsssessccessnesnseseneccaceneeneserseesececsessccaassecassasseeaeeuasanasevasenss 808
Problems ccccsccsscssscscscsssesecceseeseeencsceneenscesscesseadengeaeensnatssesaressecsesanssesereensasanesnsanes 808
Section B5 Structural and loading discontinuities ccssssceseee 815
CHAPTER 27 Closed section beams ccsssssssccssssscscssesesescnseersesseeeesneecenerersnseseneneuseseses 817
27 1 General aspects oessennneeenennntreensnenn 817
27 2 Shear stress distribution at a built-in end of a closed section beam 818
27 3 Thin-walled rectangular section beam subjected to torsion
27 4 Shear lag
Reference
Problems
CHAPTER 28 Open section beams
28 1 I-Section beam subjected t0 tOTSION «neresenseneennenensnernsenensnnensnennntnsnnessentessnsteneseenn
28 2 Torsion of an arbitrary section beam
28 3 Distributed torque loading eneneneeenennenennenen
28 4 Extension of the theory to allow for general systems of loading eessansnrernensnsstanen 873
28 5 Moment couple (bimoment)
References
Problems
Section B6 Introduction to aeroelasticity uennsuennonnennennennennernnnnnne 885
CHAPTER 29 Wing problems cee u
29 1 Types of problem csesssssssssssesssneecseenesssstsssssnceanecssesasessnseanaceeneenesssonessnerensatens
29 2 Load distribution and divergence
29 3 Control effectiveness and reversal
29 4 Introduction to “flutter” „ne
References
Problems c scccccccecsececeeressssersseesserscescesesseecsenseseseeveesneseseesesansacernecsecaesesecseaenetersneaeaes
Appendix: Design of a rear fuselage 911
Index u 939 |
| any_adam_object | 1 |
| any_adam_object_boolean | 1 |
| author | Megson, T. H. G. 1934- |
| author_GND | (DE-588)1055777008 |
| author_facet | Megson, T. H. G. 1934- |
| author_role | aut |
| author_sort | Megson, T. H. G. 1934- |
| author_variant | t h g m thg thgm |
| building | Verbundindex |
| bvnumber | BV047551996 |
| callnumber-first | T - Technology |
| callnumber-label | TL671 |
| callnumber-raw | TL671.6 |
| callnumber-search | TL671.6 |
| callnumber-sort | TL 3671.6 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | ZO 7200 ZO 7250 ZL 3230 |
| ctrlnum | (OCoLC)1286858716 (DE-599)HEB484404512 |
| dewey-full | 629.1/3431 629.134/31 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.1/3431 629.134/31 |
| dewey-search | 629.1/3431 629.134/31 |
| dewey-sort | 3629.1 43431 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Maschinenbau / Maschinenwesen Verkehr / Transport |
| discipline_str_mv | Maschinenbau / Maschinenwesen Verkehr / Transport |
| edition | Seventh edition |
| format | Book |
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| id | DE-604.BV047551996 |
| illustrated | Illustrated |
| index_date | 2024-07-03T18:24:49Z |
| indexdate | 2024-10-30T13:01:35Z |
| institution | BVB |
| isbn | 9780128228685 0128228687 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-032927613 |
| oclc_num | 1286858716 |
| open_access_boolean | |
| owner | DE-860 DE-83 |
| owner_facet | DE-860 DE-83 |
| physical | xv, 944 Seiten Illustrationen, Diagramme |
| publishDate | 2022 |
| publishDateSearch | 2022 |
| publishDateSort | 2022 |
| publisher | Elsevier, Butterworth-Heinemann |
| record_format | marc |
| series2 | Aerospace engineering |
| spelling | Megson, T. H. G. 1934- Verfasser (DE-588)1055777008 aut Aircraft structures for engineering students T.H.G. Megson Seventh edition Amsterdam Elsevier, Butterworth-Heinemann [2022] © 2022 xv, 944 Seiten Illustrationen, Diagramme txt rdacontent n rdamedia nc rdacarrier Aerospace engineering Forthcoming publication Airframes Structural analysis (Engineering) Airframes -- Textbooks Structural analysis (Engineering) -- Textbooks Flugzeugbau (DE-588)4154782-2 gnd rswk-swf Flugzeugbau (DE-588)4154782-2 s DE-604 Erscheint auch als Online-Ausgabe 978-0-32390211-3 HEBIS Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=032927613&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Megson, T. H. G. 1934- Aircraft structures for engineering students Airframes Structural analysis (Engineering) Airframes -- Textbooks Structural analysis (Engineering) -- Textbooks Flugzeugbau (DE-588)4154782-2 gnd |
| subject_GND | (DE-588)4154782-2 |
| title | Aircraft structures for engineering students |
| title_auth | Aircraft structures for engineering students |
| title_exact_search | Aircraft structures for engineering students |
| title_exact_search_txtP | 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 Structural analysis (Engineering) Airframes -- Textbooks Structural analysis (Engineering) -- Textbooks Flugzeugbau (DE-588)4154782-2 gnd |
| topic_facet | Airframes Structural analysis (Engineering) Airframes -- Textbooks Structural analysis (Engineering) -- Textbooks Flugzeugbau |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=032927613&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT megsonthg aircraftstructuresforengineeringstudents |