EXCITATION OF LOCALIZED WAVE PACKET IN 3D SUPERSONIC BOUNDARY LAYER

Alex A. Yatskih
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
2. Novosibirsk State University Novosibirsk, Russian Federation
yatskikh@itam.nsc.ru
Marina S. Rumenskikh
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
2. Novosibirsk State University Novosibirsk, Russian Federation
Yuri G. Yermolaev
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
2. Novosibirsk State University Novosibirsk, Russian Federation
yermol@itam.nsc.ru
The material was received by the Editorial Board: 30.01.2017
The results of experimental study of excitation of localized in time and space controlled disturbances (wave packets) in a supersonic swept-wing boundary layer are presented. The experiments were performed at Mach number M = 2 on the model of wing with a lenticular profile and a 40 degrees sweep angle of the leading edge at zero angle of attack. Wave packets were generated by a pulse electric discharge on the surface of the model. A structure of controlled wave packet was studied. It was found that the wave packet has an asymmetric shape. Comparison with the case of twodimensional boundary layer was done.

Keywords:
supersonic flow, controlled experiment, 3D boundary layer, swept wing, wave packet, hot-wire measurements.
УДК 532.526

EXCITATION OF LOCALIZED WAVE PACKET IN 3D SUPERSONIC BOUNDARY LAYER
References: Yatskikh A. A., Rumenskikh M. S., Yermolaev Yu. G., Kosinov A. D., Semionov N. V., Kosorygin V. S. EXCITATION OF LOCALIZED WAVE PACKET IN 3D SUPERSONIC BOUNDARY LAYER. Siberian Journal of Physics . 2017, vol. 12, no. 1. P. 57–65. (in Russ.). DOI: 10.54362/1818-7919-2017-12-1-57-65