A NUMERICAL METHOD FOR CALCULATING THE PRESSURE DUE TO THICKNESS ON SYMMETRICAL WINGS AT ZERO INCIDENCE IN SUPERSONIC FLOW
By: Eldridge,R H.
Contributor(s): Walkden,F.
Material type:
BookPublisher: Her Majesty'S Stationery Office, London 1968Description: 49.DDC classification: ARC | R&M 3535
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | ARC R&M 3535 (Browse shelf) | Not for loan Untraceable | TR17086 |
Total holds: 0
Bound With Arc R&M3533,3542-49 Lack No.3534,3536-41,3547
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