000 | 03754mm a2200721a 44500 | ||
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001 | NM002962 | ||
003 | AR-HaUTN | ||
007 | ta | ||
008 | 22020s1973 ||||||||||||||000 | spa|| | ||
005 | 20240912185429.0 | ||
040 | _aAR-HaUTN | ||
100 |
_aBruhn, E. F. b... [et al.] _97715 |
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245 |
_aAnalysis and design of flight vehicle structures _cE. F. Bruhn |
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250 | _a[2nd?] ed. | ||
260 |
_a[Carmel] _bJacobs |
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300 |
_aca. 950 p. _bil. byn, cuadros, gráficos, tablas |
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500 | _aPaginación por capítulos | ||
505 | _tThe work of the aerospace structures engineer | ||
505 | _tEquilibrium of force systems. Truss structures. Externally braced wings. Landing gear | ||
505 | _tProperties of sections. Centroids, moments of inertia, etc. | ||
505 | _tGeneral loads on aircraft | ||
505 | _tBeams. Shear and moments. Beam. Column moments | ||
505 | _tTorsion. Stresses and deflections | ||
505 | _tDeflections of structures. Castigliano's theorem. Virtual work. Matrix methods | ||
505 | _tStatically indeterminate structures. Theorem of least work. Virtual work. Matrix methods | ||
505 | _tBending moments in frames and rings by elastic center method | ||
505 | _tColumn analogy method | ||
505 | _tContinuous structures. Moment distribution method | ||
505 | _tSlope deflection method | ||
505 | _tBending stresses | ||
505 | _tBending shear stresses. Solid and open section. Shear center | ||
505 | _tShear flow in closed thinwalled sections | ||
505 | _tMembrane stresses in preasure vessels | ||
505 | _tBending of plates | ||
505 | _tTheory of the instability of columns and thin sheets | ||
505 | _tIntroduction to wing stress analysis by modified beam theory | ||
505 | _t Introduction to fuselage stress analysis by modified beam theory | ||
505 | _tLoads and stresses on ribs and frames | ||
505 | _tAnalysis of special wing problems. Cutouts. Shear lag. Swept wing | ||
505 | _tAnalysis by the "Method of displacement" | ||
505 | _tThe 3Dimensional equations of thermoelasticity | ||
505 | _tThe 2Dimensional equations of elasticity and thermoelasticity | ||
505 | _tSelected problems in elasticity and thermoelasticity | ||
505 | _tBasic principles and definitions [In flight vehicle materials and their properties] | ||
505 | _tMechanical and physical properties of metallic materials for flight vehicle structures | ||
505 | _tCombined stresses. Theory of yield and ultimate failure | ||
505 | _tStrength of columns with stable cross sections | ||
505 | _tYield and ultimate strength in bending | ||
505 | _tStrength and design of round, streamline, oval and square tubing in tension, compression, bending, torsion and combined loadings | ||
505 | _tBuckling strength of flat sheet in compression. Shear, bending and under combined stress systems | ||
505 | _tLocal buckling stress for composite shapes | ||
505 | _tCrippling strength of composite shapes and sheetstifenner panels in compression. Column strength | ||
505 | _tBuckling strength of monocoque cylinders | ||
505 | _tBuckling strength of curved sheet panels and spherical plates. Ultimate strength of stiffened curved sheet structures | ||
505 | _tDesign of metal beams. Web shear resistant (Nonbuckling) type. Part 1 : Flat sheet web with vertical stiffeners. Part 2 : Other types of nonbuckling webs | ||
505 | _tDiagonal semitension field design. Part 1 : Beams with flat webs. Part 2 : Curved web systems | ||
505 | _tSandwich construction and design | ||
505 | _tFatigue | ||
505 | _tFittings and connections. bolted and riveted | ||
505 | _tWelded connections | ||
505 | _tSome important details in structural design | ||
942 | _cBK | ||
999 |
_c2962 _d2962 |