Dore, Frank John (1947) The design of tailless airplanes. Engineer's thesis, California Institute of Technology. http://resolver.caltech.edu/CaltechETD:etd-12092008-152833
This paper reviews the various sources of information pertaining to the design of tailless airplanes. The particular topic of any report or memorandum is illustrated by its application to the problems encountered in the design of a given airplane. The subjects mentioned are the determination of the sweepback angle, aspect ratio, taper ratio, twist, dihedral, airfoil section, spanwise loading, and aerodynamic center of the wing; the control elements; and the fuselage and fillet for high speed aircraft. To illustrate the application of the source material the design of a tailless supersonic airplane is considered. The slow speed wind tunnel tests of the 1/12-scale model are included in the report.
|Item Type:||Thesis (Engineer'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 1947|
|Default Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Imported from ETD-db|
|Deposited On:||08 Jan 2009|
|Last Modified:||27 Jan 2017 18:02|
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