ON THE CONTRIBUTION OF TURBULENT BOUNDARY LAYERS TO THE NOISE INSIDE A FUSELAGE
By: Corcos,G M.
Contributor(s): Liepmann,H W.
Material type: BookPublisher: National Advisory Committee For Aeronautics, Washington,D.C. 1956Description: 43.DDC classification: NACA | TM-1420Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | General Stacks | NACA TM-1420 (Browse shelf) | Not for loan | 17288 |
Total holds: 0
Bound With Naca Tm-1421-1429.
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