Published May 6, 2015
| Submitted
Report
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The Effect of Aspect Ratio on the Lift of Flat Planing Surfaces
- Creators
- Perry, Byrne
Abstract
Previous theories and empirical formulas for the lift of flat planing surfaces are reviewed, and the resemblance of the planing surface to the airfoil noted, A simple expression, which converges to the correct limits for exactly known cases, is assumed for the ratio of planing to airfoil lift, and the planing lift is then estimated by using airfoil experimental data. The resulting calculated values are in satisfactory agreement with planing experiments.
Additional Information
Department of the Navy Office of Naval Research Contract N6onr-24424 Project NR 234-001. Report No. E-24.5.Attached Files
Submitted - E-24.5.pdf
Files
E-24.5.pdf
Files
(5.7 MB)
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Additional details
- Eprint ID
- 57305
- Resolver ID
- CaltechAUTHORS:20150506-164503104
- N6onr-24424
- Office of Naval Research (ONR)
- Created
-
2015-05-06Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Hydrodynamics Laboratory