| J. Bridges and C. A. Brown. Parametric testing of chevrons on single flow hot jets. NASA TM, 2004-213107, 2004. | |
| J. C. Lin. Review of research on low-profile vortex generators to control boundary-layer separation. Progress in Aerospace Sciences, 38: 389-420, 2002. CrossRef | |
| D. Papamoschou. Parametric study of fan flow deflectors for jet noise suppression. American Institute of Aeronautics and Astronautics Paper 2005-2890, 2005. | |
| O. H. Rask, E. Gutmark, and S. Martens. Near field acoustics of core and fan chevron nozzles. American Institute of Aeronautics and Astronautics Paper 2007-0437, 2007. | |
| P. N. Shah, P. Atsavapranee, T. Y. Hsu, T. Wei, and J. McHugh. Turbulent transport in the core of a trailing half-delta-wing vortex. Journal of Fluid Mechanics, 387: 151-175, 1999. CrossRef | |
| S. Tigglebeck, N. K. Mitra, and M. Fiebig. Experimental investigations of heat transfer enhancement and flow losses in a channel with double rows of longitudinal vortex generators. International Journal of Heat and Mass Transfer, 36: 2327-2337, 1993. CrossRef |
New Vortex Generator Design for Nozzle Internal Modification
Praveen PanickarRelated information
1 Fluid Dynamics Research Center, Illinois Institute of Technology, Chicago, IL 60616 USA
, S. SharmaRelated information1 Fluid Dynamics Research Center, Illinois Institute of Technology, Chicago, IL 60616 USA
, Shekhar SarpotdarRelated information1 Fluid Dynamics Research Center, Illinois Institute of Technology, Chicago, IL 60616 USA
, Ganesh RamanRelated information1 Fluid Dynamics Research Center, Illinois Institute of Technology, Chicago, IL 60616 USA
, William ButlerRelated information2 The Boeing Company, Seattle, Washington 98124