Numerical investigation of tonal airfoil self-noise generated by an acoustic feedback loop
Jones, Lloyd E. and Sandberg, Richard D. (2010) Numerical investigation of tonal airfoil self-noise generated by an acoustic feedback loop. In, Proceedings of the 16th AIAA/CEAS Aeroacoustics Conference. 16th CEAS/AIAA Aeroacoustics Conference Reston, US, American Institute of Aeronautics and Astronautics.
Download
Full text not available from this repository.
| Item Type: | Book Section |
|---|---|
| Related URLs: | |
| Subjects: | Q Science > QC Physics T Technology > TL Motor vehicles. Aeronautics. Astronautics |
| Divisions: | University Structure - Pre August 2011 > School of Engineering Sciences > Aerodynamics & Flight Mechanics |
| Item ID: | 185785 |
| Date Deposited: | 11 May 2011 08:40 |
| Last Modified: | 02 Mar 2012 13:38 |
| Contributors: | Jones, Lloyd E. (Author) Sandberg, Richard D. (Author) |
| Date: | 2010 |
| Status: | Published |
| Publisher: | American Institute of Aeronautics and Astronautics |
| URI: | http://eprints.soton.ac.uk/id/eprint/185785 |
Actions (login required)
 |
View Item |
