000 | 01206nab a22002657 4500 | ||
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001 | H620.91 DEW | ||
003 | AR-sfUTN | ||
008 | 190909b xx |||p|r|||| 00| 0 spa d | ||
040 | _cAR-sfUTN | ||
080 | _aH620.91 DEW | ||
100 | _aBaitinger, S. [and other] | ||
245 | _aEpoxy based matrix systems and adhesives for future rotor blade application | ||
336 |
_2rdacontent _atexto _btxt |
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337 |
_2rdamedia _asin mediaciĆ³n _bn |
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338 |
_2rdacarrier _avolumen _bnc |
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505 | _aFor liquid resin systems, a comparison of specific static and fatigue properties is drawn between epoxy (EP) and vinyl ester (VE) matrices. By the example of a 40 m rotor blade it could be demonstrated that under consideration of the better transverse strength of an UD-laminate in EP compared to VE, the rotor blade mass for the latter would have to be nearly 8 p.c. higher to have the same out-of-plane deflection at extreme load. | ||
650 | _aWIND ENERGY | ||
650 | _aEPOXY | ||
650 | _aMATRIX SYSTEMS | ||
650 | _aADHESIVES | ||
650 | _aROTOR BLADE APPLICATION | ||
773 |
_tDewi Magazin _wH620.91 DEW _nS.T.:H620.91 DEW PP0500 _g(nro. 34, Feb. 2009), p. 16-22 |
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942 | _cAN | ||
999 |
_c23727 _d23727 |