AIP Conference Proceedings
 2021
DOI: 10.1063/5.0051932
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Experimental study of the laminar-turbulent transition in the boundary layer of the wing with a sweep angle of the leading edge of 72 degrees at Mach 4

V. L. Kocharin1,
A. A. Yatskikh2,
Н. В. Семёнов3
et al.
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