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Boundary layer induced noise in aircraft, part II: the trimmed flat plate model

Graham, WR (1996) Boundary layer induced noise in aircraft, part II: the trimmed flat plate model. Journal of Sound and Vibration, 192. pp. 121-138. ISSN 0022-460X

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Item Type: Article
Subjects: UNSPECIFIED
Divisions: Div A > Fluid Mechanics
Depositing User: Cron Job
Date Deposited: 07 Mar 2014 11:51
Last Modified: 17 Apr 2014 19:04
DOI:

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