000 00631nam a22002057a 4500
003 OSt
005 20220901151535.0
008 220901b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aSewall, John L.
245 _aVibration analysis of cylindrically curved panels with simply supported or clamped edges and comparison with some experiments
_cJohn L. Sewall
260 _aWashington
_bNASA
_c1967
300 _a48p
440 _aNASA Technical Note
500 _aTechnical Reports D-3791-3800 Bound Vol. No.67635
650 _aAerodynamics
650 _aAeronautics
942 _cTR
999 _c566036
_d566036