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Virginia Tech

Efficient and robust design optimization of transonic airfoils

Abstract

dc:description.abstract

Numerical optimization procedures have been employed for the design of airfoils in transonic flow based on the transonic small-disturbance (TSD) and Euler equations. A sequential approximation optimization technique was implemented for solving the design problem of lift maximization with wave drag and area constraints. A simple linear approximation was utilized for the approximation of the lift. Accurate approximations for sensitivity derivatives of the wave drag were obtained through the utilization of Nixon's coordinate straining approach. A modification of the Euler surface boundary conditions was implemented in order to efficiently compute design sensitivities without recreating the grid. Our design procedures experienced convergence problems for some TSD solutions, where the wave drag was found not to vary smoothly with the design parameters and consequently create local optimum problems. A procedure interchanging the role of the objective function and constraint, initially minimizing drag with a constraint on the lift was found to be effective in producing converged designs, usually in approximately 10 global iterations. This procedure was also shown to be robust and efficient for cases where the drag varied smoothly, such as with the Euler solutions. The direct lift maximization with move limits which were fixed absolute values rather than fractions of the design variables, was also found to be a reliable and efficient procedure for designs based upon the Euler equations.

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
1991

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Joh, Changyeol
Committee members dc:contributor.committeemember
  • Grossman, Bernard M.
  • Haftka, Raphael T.
  • Schetz, Joseph A.
  • Walters, Robert W.
  • Mook, Dean T.

Rights

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

Identifiers

dc:identifier.*
Dc Identifier Other
etd-10192005-113327
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/39983

Chain of custody

source
Harvested from
Virginia Tech
Base URL
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Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Joh, Changyeol. Efficient and robust design optimization of transonic airfoils. doctoral thesis, Virginia Tech, 1991. http://hdl.handle.net/10919/39983