Investigation of acceleration effects on missile aerodynamics using computational fluid dynamics

I. M.A. Gledhill, K. Forsberg, P. Eliasson, J. Baloyi, J. Nordström

Research output: Contribution to journalArticlepeer-review

15 Citations (Scopus)

Abstract

In this paper we describe the implementation and validation of arbitrarily moving reference frames in the block-structured CFD-code EURANUS. We also present results from calculations on two applications involving accelerating missiles with generic configurations. It is shown that acceleration affects wave drag significantly. Also, it is shown that strake-generated vortices move significantly in turns. These results clearly show the necessity of including the acceleration effects in the calculations.

Original languageEnglish
Pages (from-to)197-203
Number of pages7
JournalAerospace Science and Technology
Volume13
Issue number4-5
DOIs
Publication statusPublished - Jun 2009
Externally publishedYes

Keywords

  • Acceleration
  • Aerodynamics
  • CFD
  • Drag
  • Vortex

ASJC Scopus subject areas

  • Aerospace Engineering

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