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References (7)
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Reibert MS Radeztsky RH (1994)
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R. Radeztsky, Mark Reibert, W. Saric (1994)
Development of Stationary Crossflow Vortices on a Swept Wing -
H. Reed, W. Saric, D. Arnal (1996)
Linear Stability Theory Applied to Boundary LayersAnnual Review of Fluid Mechanics, 28
- Publisher
- Springer Journals
- Copyright
- 1998 Chinese Society of Theoretical and Applied Mechanics
- ISSN
- 0567-7718
- eISSN
- 1614-3116
- DOI
- 10.1007/BF02487744
- Publisher site
- See Article on Publisher Site
Abstract
Abstract Crossflow instability plays very important role in the transition of the boundary layer on a swept wing, typical in the engineering applications. Experiments revealed that the linear stability theory well predicted the form of the crossflow vortices, but usually much overpredicted their growth rate. Using nonlinear theory of hydrodynamic stability, combined with some other considerations, we were able to obtain the growth rate in good agreement with experimental observations.
Journal
"Acta Mechanica Sinica" – Springer Journals
Published: May 1, 1998