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 |