000			02927cam a22004577i 4500
001			11775
003			MEMOS
005			20240731094847.0
008			180519s2017 ne a 001 0 eng d
010			_a 2016461697
020			_a9780081009147 _q(paperback)
020			_a0081009143 _q(paperback)
035			_a(OCoLC)ocn954224012
040			_aMEMOS _beng _cYDXCP _erda _dMEMOS _dSHS _dLTSCA _dOCLCF _dZWZ _dLIP _dVLB _dDLC
042			_alccopycat
050	0	0	_aTL671.6 _b.M36 2017
082	0	4	_a629.1/3431 _223 _bM497
100	1		_aMegson, T. H. G. _q(Thomas Henry Gordon), _eauthor.
245	1	0	_aAircraft structures for engineering students / _cT.H.G. Megson.
250			_aSixth edition.
260			_aLondon: _bButterworth-Heinemann is an imprint of Elsevier, _c[2017]
264			_a _a _b _c
300			_axvii, 891 pages : _billustrations ; _c24 cm.
336			_atext _btxt _2rdacontent
337			_aunmediated _bn _2rdamedia
338			_avolume _bnc _2rdacarrier
490	1		_aElsevier aerospace engineering series
500			_aIncludes index.
505	0		_aPart 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	_aAirframes _vTextbooks.
650		0	_aStructural analysis (Engineering) _vTextbooks.
650		7	_aAirframes. _2fast _0(OCoLC)fst00802910
650		7	_aStructural analysis (Engineering) _2fast _0(OCoLC)fst01135602
650		7	_aAvions _xConception et construction. _2ram
650		7	_aAvions _xVibrations. _2ram
655		7	_aTextbooks. _2fast _0(OCoLC)fst01423863
830		0	_aElsevier aerospace engineering series.
906			_a39867 _b _c _d _e _f _g
942			_2ddc _cBK _n0
999			_c15031 _d15031