000 00487pam a2200145a 44500
082 _aARC
_bR&M 3535
100 _aEldridge,R H
245 1 _aA NUMERICAL METHOD FOR CALCULATING THE PRESSURE DUE TO THICKNESS ON SYMMETRICAL WINGS AT ZERO INCIDENCE IN SUPERSONIC FLOW
260 _a
_bHer Majesty'S Stationery Office, London
_c1968
300 _a49
500 _aBound With Arc R&M3533,3542-49 Lack No.3534,3536-41,3547
700 _aWalkden,F
964 _gCIRC
997 _aTR17086 C
999 _c401053
_d401053