000 00511pam a2200145a 44500
082 _aTR
_bTR0092
100 _aHyghes,P. C.
245 1 _aSUBSONIC TESTS IN FREE MOLECULE FLOW ON IMPACT TUBE PRESSURE PROBES HAVING A WIDE RANGE OF TUBE LENGTHS AT ANGLES OF ATTACK UP TO 90%
260 _a
_bUniversity Of Toronto,Toronto
_c1965
300 _a21
440 _aUniversity Of Toronto Institute For Aerospace Studies,Report No.92
_v
500 _aBound With: Ias,Ut-86-92
964 _gCIRC
997 _aTR5053 C
999 _c392493
_d392493