000 00603nam a22001697a 4500
005 20210216124012.0
008 210216b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aAllen,H.Julian
245 _aCalculation of the chordwise load distribution over airfoil sections with plain,split,or serially hinged traniling-edge flaps[R.No.634]
_cH.Julian Allen
260 _aWashington,D.C.
_bNational Advisory Committee For Aeronautics
_c1938
300 _a16p.
440 _aNational Advisory Committee For Aeronautics(NACA)
650 _aCalculation
942 _cREF
999 _c564090
_d564090