SUBSONIC TESTS IN FREE MOLECULE FLOW ON IMPACT TUBE PRESSURE PROBES HAVING A WIDE RANGE OF TUBE LENGTHS AT ANGLES OF ATTACK UP TO 90%
By: Hyghes,P. C.
Material type:
BookSeries: University Of Toronto Institute For Aerospace Studies,Report No.92. Publisher: University Of Toronto,Toronto 1965Description: 21.DDC classification: TR | TR0092
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | TR TR0092 (Browse shelf) | Not for loan Untraceable | TR5053 |
Total holds: 0
Bound With: Ias,Ut-86-92
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