000 | 01559nam a22004337a 4500 | ||
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001 | NM003184 | ||
003 | AR-HaUTN | ||
007 | ta | ||
008 | 73020s1942 ||||||||||||||000 | spa|| | ||
005 | 20240930172302.0 | ||
040 | _aarhautn | ||
100 |
_aYounger, John E. _97928 |
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245 |
_aMechanics of aircraft structures _cJohn E. Younger |
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250 | _a2nd ed. | ||
260 |
_aNew York _bMcGraw-Hill |
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300 | _a396 p. | ||
500 | _aPublicado previamente bajo el tÃtulo "Structural design of metal airplanes" | ||
505 | _tDesign requirements | ||
505 | _tMaterials of fabrication | ||
505 | _tSumary of basic stress formulas | ||
505 | _tStructures, past, present, future | ||
505 | _tProperties of structural sections | ||
505 | _tFundamentals of structural analysis | ||
505 | _tBeams, columns, and beam columns | ||
505 | _tContinuous beams and continuous beam columns | ||
505 | _tAnalysis of torsion members | ||
505 | _tElementary principles of design of sheet-metal construction | ||
505 | _tDesign of flat reinforced plate structures | ||
505 | _tDesign of curved reinforced plate structures | ||
505 | _tDesign of thin-walled columns and stringers | ||
505 | _tTorsional rigidity of wing box beams | ||
505 | _tIntroduction to cantilever-wing analysis | ||
505 | _tDesign of thin-sheet wing webs | ||
505 | _tIntroduction to shear lag | ||
505 | _tProblems in fuselage design | ||
505 | _tWing flutter and other structural vibrations | ||
505 | _tRiveting in aircraft construction | ||
942 | _cBK | ||
999 |
_c3184 _d3184 |