000 01559mm a2200433a 44500
001 NM003184
003 AR-HaUTN
007 ta
008 73020s1942 ||||||||||||||000 | spa||
005 20240912185434.0
040 _aarhautn
100 _aYounger, John E.
_97928
245 _aMechanics of aircraft structures
_cJohn E. Younger
250 _a2nd ed.
260 _aNew York
_bMcGraw-Hill
300 _a396 p.
500 _aPublicado previamente bajo el título "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