Research output: Contribution to journal › Article › peer-review
The influence of moderate angle-of-attack variation on disturbances evolution and transition to turbulence in supersonic boundary layer on swept wing. / Kosinov, Alexander; Semionov, Nikolai; Yermolaev, Yury et al.
In: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 234, No. 1, 01.01.2020, p. 96-101.Research output: Contribution to journal › Article › peer-review
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TY - JOUR
T1 - The influence of moderate angle-of-attack variation on disturbances evolution and transition to turbulence in supersonic boundary layer on swept wing
AU - Kosinov, Alexander
AU - Semionov, Nikolai
AU - Yermolaev, Yury
AU - Smorodsky, Boris
AU - Kolosov, Gleb
AU - Yatskikh, Aleksey
AU - Semenov, Alexander
N1 - Publisher Copyright: © IMechE 2019. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2020/1/1
Y1 - 2020/1/1
N2 - The paper is devoted to an experimental and theoretical study of effect of moderate angle-of-attack variation on disturbances evolution and laminar-turbulent transition in a supersonic boundary layer on swept wing at Mach 2. Monotonous growth of the transition Reynolds numbers with angle of attack increasing from −2° to 2.7° is confirmed. For the same conditions, calculations based on linear stability theory are performed. The experimental and computational results show a favourable comparison.
AB - The paper is devoted to an experimental and theoretical study of effect of moderate angle-of-attack variation on disturbances evolution and laminar-turbulent transition in a supersonic boundary layer on swept wing at Mach 2. Monotonous growth of the transition Reynolds numbers with angle of attack increasing from −2° to 2.7° is confirmed. For the same conditions, calculations based on linear stability theory are performed. The experimental and computational results show a favourable comparison.
KW - angle of attack
KW - experiment
KW - hot-wire measurements
KW - Supersonic boundary layer
KW - swept wing
KW - NUMBER
KW - STABILITY
UR - http://www.scopus.com/inward/record.url?scp=85067801159&partnerID=8YFLogxK
U2 - 10.1177/0954410019852804
DO - 10.1177/0954410019852804
M3 - Article
AN - SCOPUS:85067801159
VL - 234
SP - 96
EP - 101
JO - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
JF - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
SN - 0954-4100
IS - 1
ER -
ID: 20655805