Analysis of unsteady aerodynamics of airfoils by rans based CFD

E. Dumlupinar, V. R. Murthy

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this work, the transonic unsteady aerodynamics calculations associated with simple harmonic pitching, indicial response to a step change in angle of attack, for NACA 64A010 airfoil are computed using CFD based on RANS. The parametric effect of Spalart-Allmaras and SST-kω turbulence models on the unsteady aerodynamics of airfoils is investigated. These results are compared with the available experimental results together with the inviscid solutions.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - 25th AIAA Applied Aerodynamics Conference, 2007
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages1128-1139
Number of pages12
ISBN (Print)1563478986, 9781563478987
DOIs
StatePublished - Jan 1 2007
Event25th AIAA Applied Aerodynamics Conference, 2007 - Miami, FL, United States
Duration: Jun 25 2007Jun 28 2007

Publication series

NameCollection of Technical Papers - AIAA Applied Aerodynamics Conference
Volume2
ISSN (Print)1048-5953

Other

Other25th AIAA Applied Aerodynamics Conference, 2007
Country/TerritoryUnited States
CityMiami, FL
Period6/25/076/28/07

ASJC Scopus subject areas

  • Engineering(all)

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