Summary
The present paper suggests a method of introducing the artificial regulable disturbances into supersonic boundary layer with the help of a point source of disturbances. While using the technique suggested the experimental study of development of a spatial wave packet of a small intensity was carried out in the boundary layer of a flat plate.
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References
Gaponov, S.A.; Maslov, A.A.: Disturbance propagation in compressible flows (in Russian). Novosibirsk: Nauka 1980.
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© 1985 Springer-Verlag, Berlin, Heidelberg
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Kosinov, A.D., Maslov, A.A. (1985). Development of Artificially Excited Disturbances in Supersonic Boundary Layer. In: Kozlov, V.V. (eds) Laminar-Turbulent Transition. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-82462-3_74
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DOI: https://doi.org/10.1007/978-3-642-82462-3_74
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-82464-7
Online ISBN: 978-3-642-82462-3
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