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