Static and dynamic analysis of a typical wing section with leading edge-trailing edge control surface configuration /

Aeroelastic phenomena have been studied for many years and their effects on flexible structures are well documented. These phenomena are investigated in the following research in a two-fold investigation. The first investigation examines the static characteristics of a wing section with a full span...

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Bibliographic Details

Main Author:	Platanitis, George, 1974-
Format:	Thesis Book
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 2003.
Subjects:	Major aerospace engineering.
Online Access:	http://proxy.library.tamu.edu/login?url=http://proquest.umi.com/pqdweb?did=765867421&sid=1&Fmt=2&clientId=2945&RQT=309&VName=PQD