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Navier-stokes computations for body/cruciform gridfin configuration

Herng Lin, Juan Cheng Huang, Ching-Chang Chieng

Research output: Chapters, Conference Papers, Creative and Literary WorksRGC 32 - Refereed conference paper (with host publication)peer-review

Abstract

A grid fin is an unconventional aerodynamic lifting and control device consisting of an outer frame with internal grid framework of small chord. Present study performs the Navier-Stokes computations for the steady subsonic and supersonic turbulent flow past (a) grid fin alone (b) fin/body combination shapes. Efficient Grid-generation procedures are proposed for fin alone and for fin/body combination configurations. Full Navier-Stokes Equations with pointwise version of Baldwin-Barth one equation turbulence model are solved by an algorithm in a fully coupled, implicit, and large block structure. The computed results are in good agreement with the experimental data and detailed shock-shock interaction structure near grid fins can be obtained and examined. © 2002 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Original languageEnglish
Title of host publication20th AIAA Applied Aerodynamics Conference
Publication statusPublished - 2002
Externally publishedYes
Event20th AIAA Applied Aerodynamics Conference 2002 - St. Louis, MO, United States
Duration: 24 Jun 200226 Jun 2002

Conference

Conference20th AIAA Applied Aerodynamics Conference 2002
PlaceUnited States
CitySt. Louis, MO
Period24/06/0226/06/02

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