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Characteristics of 3D instability of a 35-degree swept wing to CF and TS modes. Experiment and theory
- Source :
- AIP Conference Proceedings.
- Publication Year :
- 2016
- Publisher :
- Author(s), 2016.
-
Abstract
- An extensive experimental investigation of linear evolution of Cross-Flow (CF) and Tollmien-Schlichting (TS) modes of 3D boundary layer oscillations on a swept wing has been carried out. TS-instability characteristics have been studied experimentally for the first time. The characteristics of development of the two kinds of instability modes are compared with calculations and display a very good agreement. The whole dataset may be used for promotion of theoretical methods of investigation of laminar-turbulent transition in swept wing boundary layers.
Details
- ISSN :
- 0094243X
- Database :
- OpenAIRE
- Journal :
- AIP Conference Proceedings
- Accession number :
- edsair.doi.dedup.....a92c5cb0bbdde81df273ed957108d48a