000			00473pam a2200145a 44500
082			_aTR _bIOA-58
100			_aSonin,A. A.
245	1		_aLONGMUIR PROBE MEASUREMENTS IN THE STAGNATION POINT BOUNDARY LAYER OF A BLUNT-NOSED BODY IN A SUPERSONIC PLASMA FLOW
260			_a _bUniversity Of Toronto, Toronto _c1963
300			_a23
440			_aInstitute Of Aerophysics Technical Note _vNo.58
500			_aBound With: Ioa Uot 53-61
964			_gCIRC
997			_aTR5024 C
999			_c392263 _d392263