000 00453pam a2200133a 44500
082 _aRSM3751
100 _aLedger, J.A.
245 1 _aCOMPUTATION OF THE VELOCITY FIELD INDUCED BY A PLANAR SOURCE DISTRIBUTION APPROXIMATING A SYMMETRICAL NONLIFTING WING IN SUBSONIC FLOW
260 _a
_b
_c
440 _aAeronautical Research Council Reports And Memoranda
_vNo. Rsm3751
500 _aBound With: Arc 3749-3759
964 _gCIRC
997 _aTR6184 C
999 _c392144
_d392144