Investigation of various parametric geometry representation methods for airfoils

Yanping Liao*, Li Liu, Teng Long

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

5 Citations (Scopus)

Abstract

This paper presents the investigation of typical parametric geometry representation methods for airfoils, namely, PARSEC method, orthogonal basis function method and CST method. The investigation assesses the fitting accuracy of these parametric methods for various airfoils including the symmetric airfoil, cambered airfoil and supercritical airfoil. The design variables of these parametric methods are solved by the methods of least squares fit. The fitting results show that the fitting accuracy of CST method is better than other parametric methods for airfoil. The aerodynamics analysis models of these typical parametric geometry representation methods for airfoil are constructed. The pressure distributions calculated for different parametric methods are compared with the corresponding experimental pressure distributions for the actual airfoil geometry.

Original languageEnglish
Title of host publicationMechanical and Aerospace Engineering
Pages3040-3046
Number of pages7
DOIs
Publication statusPublished - 2012
Event2nd International Conference on Mechanical and Aerospace Engineering, ICMAE 2011 - Bangkok, Thailand
Duration: 29 Jul 201131 Jul 2011

Publication series

NameApplied Mechanics and Materials
Volume110-116
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2nd International Conference on Mechanical and Aerospace Engineering, ICMAE 2011
Country/TerritoryThailand
CityBangkok
Period29/07/1131/07/11

Keywords

  • CST
  • Fitting accuracy
  • Orthogonal basis function
  • PARSEC
  • Pressure distributions

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