000			01355nam a2200325 a 4500
005			20250930093239.0
008			981208s1971 us 00| 0 eng d
010			_a74-152130
020			_a0803100728
039		9	_a200805261049 _bruzita _c200805220916 _druzita _y08-18-1999 _zload
090			_aTL671.6.D35
090			_aTL671.6 _b.D35
245	0	0	_aDamage tolerance in aircraft structures _ba symposium presented at the seventy-third annual meeting, American Society for Testing and Materials, Toronto, Ontario, Canada, 21-26 June 1970 / _cM.S. Rosenfeld P.C. Paris and R.J. Hebert, symposium chairmen
260			_aPhiladelphia : _bAmerican Society for Testing and Materials, _c1971
300			_a251p. : _bill. ; _c24 cm.
440			_aASTM special technical publication _v486 _953340
504			_aIncludes bibliographical references
650		0	_aAirframes _xFacture _vCongresses
650		0	_aFracture mechanics _vCongresses
700	1		_aRosenfeld, M. S.
700	1		_aParis, P. C. _q(Paul Croce), _d1930-
700	1		_aHebert, R. J.
700	2		_aAmerican Society for Testing and Materials. Committee E-9 on Fatigue
907			_a.b10498801 _b2021-05-28 _c2019-11-12
942			_c01 _n0 _kTL671.6.D35
914			_avtls000051947
991			_aFakulti Kejuruteraan
998			_al _b1999-05-08 _cm _da _feng _g _y0 _z.b10498801
999			_c51822 _d51822