Destabilisation of Stationary and Travelling Crossflow Disturbances Due to Forward and Backward Facing Steps over a Swept Wing

Author:

Cooke Emma E.,Mughal Shahid,Sherwin Spencer,Ashworth Richard,Rolston Stephen

Publisher

Springer International Publishing

Reference20 articles.

1. Ashworth, R., Lawson, S., Lowry, R., Martinez-Cava, A., Mughal, S., Roland, H., Thomas, C.: Numerical and experimental study of the tolerance of natural laminar flow on a wing to ts destabilisation at the leading edge /wing-box junction. Royal Aeronautical Society Applied Aerodynamics Paper, pp. 336–349 (2016)

2. Bertolotti, F.P.: Linear and nonlinear stability of boundary layers with streamwise varying properties. Ph.D. thesis, Ohio State University (1991)

3. Cooke, E.E., Mughal, M.S., Sherwin, S.J., Ashworth, R., Rolston, S.: Destabilization of stationary and traveling crossflow disturbances due to steps over a swept wing. AIAA Paper (3533) (2019). https://doi.org/10.2514/6.2019-3533

4. Eppink, J.: Stereo particle image velocimetry measurements of transition downstream of a forward-facing step in a swept-wing boundary layer. AIAA Paper (0306) (2017). https://doi.org/10.2514/6.2017-0306

5. Eppink, J.: The effect of forward-facing steps on stationary crossflow instability growth and breakdown. AIAA Paper (0817) (2018). https://doi.org/10.2514/6.2018-0817

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