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Numerical Study of the Evolution of Disturbances Generated by Roughness Elements in a Supersonic Boundary Layer on a Blunted Cone. / Khotyanovsky, D. V.; Kirilovskiy, S. V.; Poplavskaya, T. V. и др.
в: Journal of Applied Mechanics and Technical Physics, Том 60, № 3, 01.05.2019, стр. 438-450.Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
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TY - JOUR
T1 - Numerical Study of the Evolution of Disturbances Generated by Roughness Elements in a Supersonic Boundary Layer on a Blunted Cone
AU - Khotyanovsky, D. V.
AU - Kirilovskiy, S. V.
AU - Poplavskaya, T. V.
AU - Kudryavtsev, A. N.
PY - 2019/5/1
Y1 - 2019/5/1
N2 - Results of direct numerical simulations of the roughness-induced development of instability and transition to turbulence in a supersonic boundary layer on a blunted cone for the free-stream Mach number M∞ = 5.95 are presented. The flow parameters and model geometry are consistent with the conditions of the experiments performed in the study. The following roughness types are considered: random distributed roughness, isolated roughness elements of different shapes, and a group of regularly arranged roughness elements. The processes of the instability development and transition for different roughness types are compared, and possible mechanisms of the roughness influence on the stability of boundary layers on blunt bodies are discussed.
AB - Results of direct numerical simulations of the roughness-induced development of instability and transition to turbulence in a supersonic boundary layer on a blunted cone for the free-stream Mach number M∞ = 5.95 are presented. The flow parameters and model geometry are consistent with the conditions of the experiments performed in the study. The following roughness types are considered: random distributed roughness, isolated roughness elements of different shapes, and a group of regularly arranged roughness elements. The processes of the instability development and transition for different roughness types are compared, and possible mechanisms of the roughness influence on the stability of boundary layers on blunt bodies are discussed.
KW - blunted conical body
KW - direct numerical simulation
KW - distributed roughness
KW - isolated roughness elements
KW - laminar-turbulent transition
KW - supersonic boundary layer
KW - TRANSITION
KW - INSTABILITY
KW - STABILITY
KW - FLOW
UR - http://www.scopus.com/inward/record.url?scp=85073646632&partnerID=8YFLogxK
UR - https://www.elibrary.ru/item.asp?id=41697653
U2 - 10.1134/S0021894419030052
DO - 10.1134/S0021894419030052
M3 - Article
AN - SCOPUS:85073646632
VL - 60
SP - 438
EP - 450
JO - Journal of Applied Mechanics and Technical Physics
JF - Journal of Applied Mechanics and Technical Physics
SN - 0021-8944
IS - 3
ER -
ID: 24413070