Rassieur, W. T. (1934) Hinge moments. Master's thesis, California Institute of Technology. http://resolver.caltech.edu/CaltechETD:etd-04152008-090606
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|
|Thesis Availability:||Public (worldwide access)|
|Defense Date:||1 January 1934|
|Default Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Imported from ETD-db|
|Deposited On:||23 Apr 2008|
|Last Modified:||26 Dec 2012 02:37|
- Final Version
See Usage Policy.
Repository Staff Only: item control page