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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: materialTypeLabelBookPublisher: Her Majesty'S Stationery Office, London 1967Description: 30.DDC classification: ARC | C.P. 1005
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Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report 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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