000 00707 a2200265 4500
001 78569
020 _a
041 _aeng
080 _a043:629.13.011:620.168Mar
245 _aBuckling behaviour of damaged and undamged stiffened composite panels under static in-plane compression (R)
250 _a
260 _aMumbai
260 _bIIT
260 _c1999
300 _ax,88 p.
300 _c28 cm
490 _a
100 _aMarathe, M.S.
700 _aMujumdar, P.M. and Lakkad, S.C.
650 _aMujumdar, P.M. and Lakkad, S.C.
650 _aTheses and Dissertations
650 _aAircraft structures , Composite materials , Streangth of materials , Panels
942 _cTD
942 _2UDC
999 _c175737
_d175737