Citation
Rassieur, W. T. (1934) Hinge moments. Master's thesis, California Institute of Technology. http://resolver.caltech.edu/CaltechETD:etd-04152008-090606
Abstract
The matter herein presented represents the results of an investigation on hinge moments of ailerons on a 1/12.5 scale model of a main wing airfoil of the XP3D-l Navy Patrol Boat.
The data obtained were then employed in the calculation of stick forces due to aileron moments on the full scale airplane, the calculations covering a flying range of eighty to one hundred eighty miles per hour.
| Item Type: | Thesis (Master's thesis) |
|---|---|
| Degree Grantor: | California Institute of Technology |
| Division: | Engineering and Applied Science |
| Major Option: | Aeronautics |
| Thesis Availability: | Public (worldwide access) |
| Research Advisor(s): |
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| Thesis Committee: |
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| Defense Date: | 1 January 1934 |
| Record Number: | CaltechETD:etd-04152008-090606 |
| Persistent URL: | http://resolver.caltech.edu/CaltechETD:etd-04152008-090606 |
| Default Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. |
| ID Code: | 1394 |
| Collection: | CaltechTHESIS |
| Deposited By: | Imported from ETD-db |
| Deposited On: | 23 Apr 2008 |
| Last Modified: | 26 Dec 2012 02:37 |
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