000 00444pam a2200121a 44500
082 _aC.P.
_b582
100 _aLawlor,E F
245 1 _aWIND TUNNEL TESTS AT MACH NUMBERS BETWEEN 0.6 AND 1.4 OF A 60 DEGREE SWEPT WING HAVING AN AEROFOIL SECTION DESIGNED FOR SUBCRITICAL FLOW AT A MACH NUMBER OF 1.2
260 _a
_bHer Majesty'S Stationery Office, London
_c1962
500 _aBound With C.P.581, 583-590
964 _gCIRC
997 _aTR10471 C
999 _c395441
_d395441