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 |