Numerical Simulation on Circular-Arc Grid-Fin Configurations

Article Preview

Abstract:

A grid fin is an unconventional lifting and control surface which consists of an outer frame with an inner grid of intersecting planar surfaces of small chord. Normal shocks form at the back of the lattice cells at transonic Mach numbers thus choking the flow through the cells and causing a significant reduction in lift force and increase in drag force. An improved circular-arc grid-fin configuration is proposed in the present study to reduce transonic flow choking. Viscous computational fluid dynamic simulations were performed to investigate flows over single baseline and circular-arc grid fins and body-fin configurations under transonic and supersonic flow with Mach numbers in the range of 0.6-4.0. The present numerical results indicate the drag coefficient on single circular-arc grid fin and body-fin configuration is decreased by approximately 10%-24% and 8% respectively for all the Mach numbers investigated in the present study.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

342-346

Citation:

Online since:

October 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Hughson, M. C. ,Blades, E. L. ,and Abate, G. L. Transonic Aerodynamic Analysis of Lattice Grid Tail Fin Missiles. AIAA Paper 2006-3651, 24th AIAA Applied Aerodynamics Conference, San Francisco, California,5-8 June (2006).

DOI: 10.2514/6.2006-3651

Google Scholar

[2] Montgomery C. Hughson, Eric L. Analysis of Lattice Grid Tailfin Missiles in High-Speed Flow. AIAA 2007-3932.

DOI: 10.2514/6.2007-3932

Google Scholar

[3] Yan Zeng, Jinsheng Cai , Marco Debiasi. Numerical Study on Drag Reduction for Grid-Fin Configurations. AIAA 2007-3932.

Google Scholar

[4] Zing, Y, Cai J S,Debiasi, M. Numerical Study on Drag Reduction for Grid-Fin Configurations. AIAA-2009-1105,(2009).

DOI: 10.2514/6.2009-1105

Google Scholar

[5] Marco Debaser,Zeng Yan. Swept-back Grid Fins for Transonic Drag Reduction. AIAA 2010-4244, (2010).

DOI: 10.2514/6.2010-4244

Google Scholar