000 | 01736nam a22004457a 4500 | ||
---|---|---|---|
001 | NM002996 | ||
003 | AR-HaUTN | ||
005 | 20240930172255.0 | ||
007 | ta | ||
008 | 12020sc. 1 ||||||||||||||000 | spa|| | ||
040 |
_aAR-HaUTN _cAR-HaUTN |
||
100 |
_aShanley, F. R. _93189 |
||
245 |
_aWeigh-tstrength analysis of aircraft structures _cF. R. Shanley |
||
250 | _a2nd ed. | ||
260 |
_aNew York _bDover |
||
300 |
_a404 p. _bgráficos |
||
500 | _aIndice alfabético, al final del libro | ||
504 | _aReferencias bibliográficas p. 387396 | ||
505 | _tMethods of analysis | ||
505 | _tPrinciples of structural design for minimun weight | ||
505 | _tGeneral instability of stiffenes shells in pure bending | ||
505 | _tMinimun weight of stiffened cylindrical shells in pure bending | ||
505 | _tEffect of torsionalstiffness requirements on wing structural weight | ||
505 | _tGeneral weightanalysis methods | ||
505 | _tWieght analysis of the sheetstringerrib type of wing structure | ||
505 | _tEffective depth of airfoil sections | ||
505 | _tEvaluation of integration factors | ||
505 | _tInertia and shear reduction factors | ||
505 | _tWing ribs and secondary structure | ||
505 | _tNon optimum structural weight | ||
505 | _tWeight analysis of the thickplate type of wing structure | ||
505 | _tWeight analysis of thinwing structures | ||
505 | _tWeight analysis of fuselage and shell structures | ||
505 | _tAnalysis of stressstraintime relations | ||
505 | _tStressstraintime properties of same aircraft materials | ||
505 | _tInelastic column theory | ||
505 | _tPrinciples of creep buckling | ||
505 | _tEffect of creep on column deflection | ||
942 |
_cBK _2udc |
||
999 |
_c2996 _d2996 |