Author:
Yatskikh A A,Ermolaev Y G,Smorodsky B V,Panina A V,Semionov N V,Kosinov A D
Abstract
Abstract
The evolution of an artificial localized wave packet in a supersonic boundary layer of a swept wing is experimentally investigated at Mach number M = 2. The wave characteristics of the development of disturbances at various frequencies are determined. The growth increments of the most increasing modes of the wave packet are estimated. Comparison with the results of calculations based on the linear theory of stability is carried out.
Subject
General Physics and Astronomy
Cited by
4 articles.
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1. Experimental investigation of natural disturbances of a supersonic boundary layer on a swept-wing model with periodic roughness at Mach 2.5;AIP Conference Proceedings;2021
2. On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2.5;AIP Conference Proceedings;2021
3. On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2;HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2020): Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, dedicated to the 90th anniversary of the birth of RI Soloukhin;2020
4. Experimental study of natural disturbances of a supersonic boundary layer on a swept-wing model with periodic roughness;HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2020): Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, dedicated to the 90th anniversary of the birth of RI Soloukhin;2020