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ON THE CONTRIBUTION OF TURBULENT BOUNDARY LAYERS TO THE NOISE INSIDE A FUSELAGE

By: Corcos,G M.
Contributor(s): Liepmann,H W.
Material type: materialTypeLabelBookPublisher: National Advisory Committee For Aeronautics, Washington,D.C. 1956Description: 43.DDC classification: NACA | TM-1420
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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 NACA TM-1420 (Browse shelf) Not for loan 17288
Total holds: 0

Bound With Naca Tm-1421-1429.

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