000 00604nam a2200193Ia 4500
919 _a151124
082 _a629.1333520153132
_bP05 "THESIS"
100 _aThakkar, Dipali
245 _aHelicopter vibration reduction using single crystal and soft piezoceramic shear induced active blade twist
_b
_cby Dipali Thakkar
260 _aBangalore
_bIISc
_c2005
300 _axix, 189p.
490 _aIISc, Dept. of AE PhD. Thesis
690 _aHelicopters-Vibration; Piezoceramics-Sheardynamics
999 _c145691
_d145691