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Virginia Tech

Sensitivity analysis of the static aeroelastic response of a wing

Abstract

dc:description.abstract

A technique to obtain the sensitivity of the static aeroelastic response of a three dimensional wing model is designed and implemented. The formulation is quite general and accepts any aerodynamic and structural analysis capability. A program to combine the discipline level, or local, sensitivities into global sensitivity derivatives is developed. A variety of representations of the wing pressure field are developed and tested to determine the most accurate and efficient scheme for representing the field outside of the aerodynamic code. Chebyshev polynomials are used to globally fit the pressure field. This approach had some difficulties in representing local variations in the field, so a variety of local interpolation polynomial pressure representations are also implemented. These panel based representations use a constant pressure value~ a bilinearly interpolated value, or a biquadratic ally interpolated value. The interpolation polynomial approaches do an excellent job of reducing the numerical problems of the global approach for comparable computational effort. Regardless of the pressure representation used, sensitivity and response results with excellent accuracy have been produced for large integrated quantities such as wing tip deflection and trim angle of attack. The sensitivities of such things as individual generalized displacements have been found with fair accuracy. In general, accuracy is found to be proportional to the relative size of the derivatives to the quantity itself.

Degree

thesis:*
Name thesis:degree_name
Ph. D.
Level thesis:degree_level
doctoral
Discipline thesis:degree_discipline
Aerospace Engineering
Department dc:contributor.department
Aerospace Engineering
Grantor dc:publisher
Virginia Tech
Year dc:date.issued
1993

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Eldred, Lloyd B.
Chair dc:contributor.committeechair
  • Kapania, Rakesh K.
Committee members dc:contributor.committeemember
  • Haftka, Raphael T.
  • Johnson, Eric R.
  • Librescu, Liviu
  • Mason, William H.

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en

Identifiers

dc:identifier.*
Dc Identifier Other
etd-10242005-174006
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/40147

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
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citation

Eldred, Lloyd B.. Sensitivity analysis of the static aeroelastic response of a wing. doctoral thesis, Virginia Tech, 1993. http://hdl.handle.net/10919/40147