000 00516pam a2200181a 44500
008 160408b1986 xxu||||| |||| 00| 0 eng d
020 _a9283515366
082 _a629.1341015
_bP881
100 _a
245 1 _aPRACTICAL APPLICATION OF FINITE ELEMENT ANALYSIS TO AIRCRAFT STRUCTURAL DESIGN
260 _aLoughton
_bAgard
_c1986
300 _a1 v.
440 _aAgard-Ls-147
_v
650 _aAirframes -- Mathematical Models
650 _aStructural Frames -- Models
964 _gCIRC
997 _aA105277 C
999 _c324977
_d324977