06.08.2013 Views

university of florida thesis or dissertation formatting template

university of florida thesis or dissertation formatting template

university of florida thesis or dissertation formatting template

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

6-27 Instantaneous Cp measurements on F-16 wing at 93% span. ...........................................130<br />

6-28 Instantaneous Cp measurements on F-16 wing at 88% span. ...........................................131<br />

6-29 Lissajous plots <strong>of</strong> upper surface Cp vs. local displacement during 1Hz pitch<br />

oscillation f<strong>or</strong> clean-wing Grid0. .....................................................................................132<br />

6-30 2-D (left column) and 3-D (right column) Lissajous f<strong>or</strong> Grid0 clean-wing 1Hz pitch<br />

oscillation case .................................................................................................................133<br />

6-31 Lissajous plots <strong>of</strong> upper surface Cp vs. local displacement during 8Hz pitch<br />

oscillation f<strong>or</strong> clean-wing Grid9. .....................................................................................134<br />

6-32 2-D (left column) and 3-D (right column) Lissajous f<strong>or</strong> Grid9 clean-wing 8Hz pitch<br />

oscillation case .................................................................................................................135<br />

6-33 Temp<strong>or</strong>al analysis <strong>of</strong> upper surface Cp f<strong>or</strong> Grid0 1Hz pitch oscillation at 93% span<br />

vs. 67% ch<strong>or</strong>d...................................................................................................................136<br />

6-34 Temp<strong>or</strong>al analysis <strong>of</strong> upper surface Cp f<strong>or</strong> Grid0 1Hz pitch oscillation at 88% span<br />

vs. 72% ch<strong>or</strong>d...................................................................................................................137<br />

6-35 Temp<strong>or</strong>al analysis <strong>of</strong> upper surface Cp f<strong>or</strong> Grid0 1Hz pitch oscillation at 88% span<br />

vs. 81% ch<strong>or</strong>d...................................................................................................................138<br />

6-36 Temp<strong>or</strong>al analysis <strong>of</strong> upper surface Cp f<strong>or</strong> Grid9 8Hz pitch oscillation at 98% span<br />

vs. 54% ch<strong>or</strong>d...................................................................................................................139<br />

6-37 Temp<strong>or</strong>al analysis <strong>of</strong> upper surface Cp f<strong>or</strong> Grid9 8Hz pitch oscillation at 93% span<br />

vs. 58% ch<strong>or</strong>d...................................................................................................................140<br />

6-38 Temp<strong>or</strong>al analysis <strong>of</strong> upper surface Cp f<strong>or</strong> Grid9 8Hz pitch oscillation at 88% span<br />

vs. 58% ch<strong>or</strong>d...................................................................................................................141<br />

6-39 DDES <strong>of</strong> F-16 in 8Hz sinusoidal pitching motion with instantaneous Mach=1<br />

boundary iso-surface col<strong>or</strong>ed by pressure ........................................................................142<br />

6-40 DDES <strong>of</strong> F-16 in 8Hz sinusoidal pitching motion with instantaneous v<strong>or</strong>ticity<br />

magnitude iso-surface col<strong>or</strong>ed by pressure ......................................................................143<br />

6-41 Instantaneous Cp Measurements on F-16 wing at 98% span ...........................................144<br />

6-42 Instantaneous Cp Measurements on F-16 wing at 93% span ...........................................145<br />

6-43 Instantaneous Cp Measurements on F-16 wing at 88% span. ..........................................146<br />

6-44 Lissajous plots <strong>of</strong> upper surface Cp vs. local displacement during 8Hz pitch<br />

oscillation f<strong>or</strong> tip-launcher Grid8. ....................................................................................147<br />

12

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!