Characteristics of 3D instability of a 35-degree swept wing to CF and TS modes. Experiment and theory

Author:

Borodulin V. I.,Ivanov A. V.,Kachanov Y. S.,Örlü R.,Hanifi A.,Hein S.

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Reference9 articles.

1. Swept-wing boundary-layer receptivity to surface non-uniformities

2. Receptivity coefficients at excitation of cross-flow waves by free-stream vortices in the presence of surface roughness

3. Receptivity of a swept-wing boundary layer to micron-sized discrete roughness elements

4. Design and Tests of Wind-Tunnel Sidewalls for Receptivity Experiments on a Swept Wing

5. A. Hanifi, S. Hein, D.G. Romano, M. Minervino, W. Würz, V.I. Borodulin, A.V. Ivanov, and Y.S. Kachanov, “Numerical and experimental realization of an infinite-swept-wing boundary-layer flow in a wind tunnel,” in Proc. 17th Int. Conf. Methods of Aerophysical Research, edited by V.M. Fomin (ITAM SB RAS, Novosibirsk, 2014), URL: http://www.itam.nsc.ru/users/libr/eLib/confer/ICMAR/2014/pdf/Hanifi%20et%20al_89.pdf

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