Fleming, Morton Klyne (1936) Experimental investigation of the effect of power upon the static longitudinal stability of a low winged monoplane and a method for its calculation. Master's thesis, California Institute of Technology. http://resolver.caltech.edu/CaltechETD:etd-04152008-085638
To obtain the change in the longitudinal moment of a low winged monoplane caused by the addition of the propulsive unit operating at various conditions of power. To construct possible working charts for use in calculating this change from power off wind tunnel tests of scale models.
|Item Type:||Thesis (Master's thesis)|
|Subject Keywords:||Aeronautical Engineering|
|Degree Grantor:||California Institute of Technology|
|Division:||Engineering and Applied Science|
|Thesis Availability:||Public (worldwide access)|
|Defense Date:||1 January 1936|
|Default Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Imported from ETD-db|
|Deposited On:||21 Apr 2008|
|Last Modified:||19 Oct 2016 22:49|
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