NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Chapter 14 - AeroelasticityFlutter is an aeroelastic phenomenon in which aerodynamic, elastic and inertia forces couple unfavorably at a sufficiently high speed to produce an unstable oscillation which may grow without limit and so result in a structural failure. Flutter is, unfortunately, not a problem that will just "go away": modern aircraft, in particular, are progressively more flexible, fly faster, and are highly control configured, more maneuverable and more system dependent. The development of active control systems for flutter suppression will actually complicate the problem by introducing a fourth "servo" dimension into the aeroelastic scene and will at best only defer flutter to higher speeds.
Document ID
20050209974
Acquisition Source
Legacy CDMS
Document Type
Other - Technical Report
Authors
J J Meijer
(National Aerospace Laboratory Amsterdam, Netherlands)
Date Acquired
August 23, 2013
Publication Date
July 1, 2005
Publication Information
Publication: Introduction to Flight Test Engineering [Introduction Aux Techniques Des Essais En Vol]
Publisher: North Atlantic Treaty Organization
Volume: 14
ISBN: 9283711262
Subject Category
Aerodynamics
Aircraft Stability and Control
Report/Patent Number
RTO-AG-300-V14
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available