000 00405pam a2200133a 44500
082 _aARC
_bC.P 1189
100 _aPortnoy,H
245 1 _aTHE EFFECT OF CONICAL THICKNESS DISTRIBUTIONS ON THE SEPRATED FLOW PAST SLENDER DELTA WINGS.
260 _a
_bHer Majesty'S Stationery Office, London
_c1971
300 _a15
500 _aBound With Arc Cp-1181-1188,1190.
964 _gCIRC
997 _aTR14462 C
999 _c397828
_d397828