000 00611pam a2200181a 44500
003 OSt
040 _cIIT Kanpur
041 _aeng
100 _aWard,John F
245 1 _aNote on helicopter rotor-blade fatigue-crack propagation rates under equivalent-lifetime fatigue loadings[NASA TN D -1018]
_cJohn F Ward
260 _a Washington, D.C.
_bNational Aeronautics and Space Adminstration
_c1962
300 _a10p
440 _aNational Aeronautics and Space Adminstration
440 _aNASA technical note
500 _aBound vol. contains D 1011-1020
650 _aHelicopter rotor-blade
942 _cTR
999 _c394303
_d394303