000 00579 a2200241 4500
001 287973
020 _a
041 _aeng
080 _aDARC CP 1372 : 1976
245 _aWind-tunnel investigation of the effects of flap span and deflection angle, wing platform and a body on the high-lift performance of a 28° swept wing
250 _a
260 _aLondon
260 _bHer Majesty's Stationary Office
260 _c1976
300 _a198 p.
300 _c
856 _uARC
490 _aARC CP 1372 : 1976
700 _a
650 _a
650 _a
942 _cPP
942 _2UDC
999 _c247643
_d247643