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Hinge moments


Rassieur, W. T. (1934) Hinge moments. Master's thesis, California Institute of Technology.


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):
  • Von Kármán, Theodore (advisor)
  • Klein, Arthur Louis (advisor)
Thesis Committee:
  • Unknown, Unknown
Defense Date:1 January 1934
Record Number:CaltechETD:etd-04152008-090606
Persistent URL:
Default Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:1394
Deposited By: Imported from ETD-db
Deposited On:23 Apr 2008
Last Modified:26 Dec 2012 02:37

Thesis Files

PDF (Rassieur_wt_1934.pdf) - Final Version
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