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035 _a(ATU)b11280517
035 _a(OCoLC)76798397
040 _aUKM
_beng
_erda
_cUKM
_dBAKER
_dBWKUK
_dYDXCP
_dOHX
_dBTCTA
_dUMC
_dOCoLC
_dATU
050 0 _aTL671.6
_b.M36 2007
082 0 _a629.13431
_222
100 1 _aMegson, T. H. G.
_q(Thomas Henry Gordon)
_eauthor.
_9231067
245 1 0 _aAircraft structures for engineering students /
_cT.H.G. Megson.
250 _aFourth edition.
264 1 _aOxford ;
_aBurlington, MA :
_bButterworth-Heinemann,
_c2007.
300 _axx, 804 pages :
_billustrations ;
_c25 cm.
336 _atext
_btxt
_2rdacontent
337 _aunmediated
_bn
_2rdamedia
338 _avolume
_bnc
_2rdacarrier
490 1 _aElsevier aerospace engineering series
500 _aPrevious ed.: London : Arnold, 1999.
504 _aIncludes bibliographical references and index.
505 0 0 _gSect. A1.
_tElasticity --
_g1.
_tBasic elasticity --
_g2.
_tTwo dimensional problems in elasticity --
_g3.
_tTorsion of solid sections --
_gSect. A2.
_tVirtual work, energy matrix methods --
_g4.
_tVirtual work and energy methods --
_g5.
_tEnergy methods --
_g6.
_tMatrix methods --
_gSect. A3.
_tThin plate theory --
_g7.
_tBending of thin plates --
_gSect. A4.
_tStructural instability --
_g8.
_tColumns --
_g9.
_tThin plates --
_gSect. A5.
_tVibration of structures --
_g10.
_tStructural vibration --
_gSect. B1.
_tPrinciples of stressed skin construction --
_g11.
_tMaterials --
_g12.
_tStructural components of aircraft --
_gSect. B2.
_tAirworthiness and airframe loads --
_g13.
_tAirworthiness --
_g14.
_tAirframe loads --
_g15.
_tFatigue --
_gSect. B3.
_tBending, shear and torsion of thin-walled beams --
_g16.
_tBending of open and closed, thin-walled beams --
_g17.
_tShear of beams --
_g18.
_tTorsion of beams --
_g19.
_tCombined open and closed section beams --
_g20.
_tStructural idealization --
_gSect. B4.
_tStress analysis of aircraft components --
_g21.
_tWing spars and box beams --
_g22.
_tFuselages --
_g23.
_tWings --
_g24.
_tFuselage frames and wing ribs --
_g25.
_tLaminated composite structures --
_gSect. B5.
_tStructural and loading discontinuities --
_g26.
_tClosed section beams --
_g27.
_tOpen section beams --
_gSect. B6.
_tIntroduction to aeroelasticity --
_g28.
_tWing problems.
520 1 _a"Aircraft Structures for Engineering Students is a self-contained text for students of aerospace and mechanical engineering. It covers all the fundamental subjects taken in an aircraft structural design and analysis course, including elasticity, structural mechanics and analysis, airworthiness and aeroelasticity. It is ideal for use as a textbook for a first course in aircraft structures or structural design and analysis, as well as a reference for graduate level courses."--BOOK JACKET.
588 _aMachine converted from AACR2 source record.
650 0 _aAirframes.
_9313601
830 0 _aElsevier aerospace engineering series.
_91064964
907 _a.b11280517
_b03-10-17
_c27-10-15
942 _cB
945 _a629.13431 MEG
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