Experimental Analysis of the Effect of Suction and Step Height on Boundary-Layer Transition

Author:

Dimond Benjamin,Costantini Marco,Klein Christian

Publisher

Springer International Publishing

Reference18 articles.

1. Arnal, D., Perraud, J., Séraudie, A.: Attachment line and surface imperfection problems. AGARD RTO-EN-AVT-151 pp. 9–1 to 9–20 (2009)

2. Braslow, A.L.: A History of Suction-Type Laminar-Flow Control with Emphasis on Flight Research, No. 13. Monographs in Aerospace History, No (1999)

3. Bushnell, D.M., Tuttle, M.H.: Survey and bibliography on attainment of laminar flow control in air using pressure gradient and suction. NASA RP 1035(1979)

4. Costantini, M.: Experimental analysis of geometric, pressure gradient and surface temperature effects on boundary-layer transition in compressible high reynolds number flows. Ph.D. thesis, RWTH Aachen (2016). http://elib.dlr.de/117965/

5. Costantini M, Hein S, Henne U, Klein C, Koch S, Schojda L, Ondrus V, Schröder W (2016) Pressure gradient and nonadiabatic surface effects on boundary layer transition. AIAA Journal 54(11), 3465–3480, doi: 10.2514/1.J054583

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