THE EFFECT OF CONICAL THICKNESS DISTRIBUTIONS ON THE SEPRATED FLOW PAST SLENDER DELTA WINGS.
By: Portnoy,H.
Material type:![materialTypeLabel](/opac-tmpl/lib/famfamfam/BK.png)
Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
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PK Kelkar Library, IIT Kanpur | General Stacks | ARC C.P 1189 (Browse shelf) | Not for loan | TR14462 |
Total holds: 0
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Bound With Arc Cp-1181-1188,1190.
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