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
Full text not available from this repository.| Item Type: | Article |
|---|---|
| Additional Information: | Publisher: Academic Press, Great Britain |
| Subjects: | UNSPECIFIED |
| Divisions: | Div A > Fluid Mechanics |
| Depositing User: | Cron Job |
| Date Deposited: | 28 Oct 2011 16:42 |
| Last Modified: | 08 Apr 2013 01:08 |
| DOI: |
Actions (login required)
| View Item |

