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 |