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The University of Arizona.

Prediction and analysis of wing flutter at transonic speeds.

Abstract

dc:description.abstract

This dissertation deals with the instability, known as flutter, of the lifting and control surfaces of aircraft of advanced design at high altitudes and speeds. A simple model is used to represent the aerodynamics for flutter analysis of a two-degree-of-freedom airfoil system. Flutter solutions of this airfoil system are shown to be algebraically homomorphic in that solutions about different elastic axes can be found by mapping them to those about the mid-chord. Algebraic expressions for the flutter speed and frequency are thus obtained. For the prediction of flutter of a wing at transonic speeds, an accurate and efficient computer code is developed. The unique features of this code are the capability of accepting a steady mean flow regardless of its origin, a time dependent perturbation boundary condition for describing wing deformations on the mean surface, and a locally applied three-dimensional far-field boundary condition for minimizing wave reflections from numerical boundaries. Results for various test cases obtained using this code show good agreement with the experiments and other theories.

Degree

thesis:*
Name thesis:degree_name
Ph.D.
Level thesis:degree_level
doctoral
Discipline thesis:degree_discipline
Aerospace and Mechanical Engineering
Grantor dc:publisher
The University of Arizona.
Year dc:date.issued
1991

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Shieh, Teng-Hua.
Advisor dc:contributor.advisor
  • Fung, K.-Y.
Committee members dc:contributor.committeemember
  • Fasel, Hermann
  • Balsa, Thomas F.
  • Brio, Moysey

Subjects

dc:subject × 5

Rights

dc:rights
Statement dc:rights
  • Copyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author.
Language dc:language.iso
en

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/10150/185694
OAI identifier oai:identifier
oai:repository.arizona.edu:10150/185694

Chain of custody

source
Harvested from
University of Arizona
Base URL
repository.arizona.edu/oai/request
Last updated
2026-07-24
Source record
OAI-PMH GetRecord
citation

Shieh, Teng-Hua.. Prediction and analysis of wing flutter at transonic speeds.. doctoral thesis, The University of Arizona., 1991. http://hdl.handle.net/10150/185694