Experimental Investigation of the Effect Of Power Upon the Static Longitudinal Stability of a Low Winged Monoplane and a Method for its Calculation

Citation

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. doi:10.7907/JKVP-P690. https://resolver.caltech.edu/CaltechETD:etd-04152008-085638

Abstract

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
Major Option:	Aeronautics
Thesis Availability:	Public (worldwide access)
Research Advisor(s):	Millikan, Clark Blanchard
Group:	GALCIT
Thesis Committee:	Unknown, Unknown
Defense Date:	1 January 1936
Record Number:	CaltechETD:etd-04152008-085638
Persistent URL:	https://resolver.caltech.edu/CaltechETD:etd-04152008-085638
DOI:	10.7907/JKVP-P690
Default Usage Policy:	No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:	1393
Collection:	CaltechTHESIS
Deposited By:	Imported from ETD-db
Deposited On:	21 Apr 2008
Last Modified:	03 Oct 2019 23:07

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