Aerostructures Test Wing

TBMG-1342

12/01/2003

Abstract
Content

The Aerostructures Test Wing (ATW) was an apparatus used in a flight experiment during a program of research on aeroelastic instabilities. The ATW experiment was performed to study a specific instability known as flutter. Flutter is a destructive phenomenon caused by adverse coupling of structural dynamics and aerodynamics. The process of determining a flight envelope within which an aircraft will not experience flutter, known as flight flutter testing, is very dangerous and expensive because predictions of the instability are often unreliable.

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Citation
"Aerostructures Test Wing," Mobility Engineering, December 1, 2003.
Additional Details
Publisher
Published
Dec 1, 2003
Product Code
TBMG-1342
Content Type
Magazine Article
Language
English