000 00387pam a2200121a 44500
008 160408b xxu||||| |||| 00| 0 eng d
082 _aTR
_bR & M-3809
100 _aP. Brotherhood
245 1 _aFlight measurements of the effects of simulated leading-edge erosion on helicopter blade stall,tarsional loads and perfarmance
260 _a
_b
_c
700 _aW. D. Brown
997 _aA58436 C
999 _c310955
_d310955