000 | 00660nam a2200193 4500 | ||
---|---|---|---|
005 | 20200706115607.0 | ||
008 | 200706b xxu||||| |||| 00| 0 eng d | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
100 | _aSchwind, R. G. | ||
245 |
_aThe effects of leading-edge serrations on Reducing flow unsteadiness about airfoils _ban experimental and analytical invertigation [NASA CR-2344] _cR. G. Schwind and H. J. Allen |
||
260 |
_aNasa _bWashington, D. C. _c1973 |
||
300 | _a97p | ||
440 | _aNational Aeronautics and Space Administration (NASA) | ||
505 | _aNASA technical report | ||
650 | _aAerofoils | ||
700 | _aAllen, H. J, | ||
942 | _cREF | ||
999 |
_c563077 _d563077 |