THE CALCULATION OF THE PRESSURE DISTRIBUTION ON A THICK CAMBERED AEROFOIL AT SUBSONIC SPEEDS INCLUDING THE EFFECTS OF THE BOUNDARY LAYER.
By: Powell,B J.
Material type: BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 30.DDC classification: ARC | C.P. 1005Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | General Stacks | ARC C.P. 1005 (Browse shelf) | Not for loan | TR10830 |
Total holds: 0
Bound With Arc C.P.1000-1004, 1006-1009
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