@inproceedings{b1e7a2f75785414d8dcd999540840dbd,
title = "Influence of small attack angles on the transition on the wing with the subsonic leading edge at M=2",
abstract = "The paper is devoted to an experimental study of laminar-turbulent transition in supersonic boundary layers on swept wings. The experiments were fulfilled in the low nose supersonic wind tunnel T-325 of Khristianovich Institute of Theoretical and Applied Mechanics on the models of a swept wing with a swept angle of 72° at Mach 2 which corresponds to a subsonic leading edge. The transition location was determined using a constant temperature hot-wire anemometer. A comparison of the influence of small angles of attack on the transition position with a model with a supersonic leading edge is shown. The transition to a wing model with a subsonic leading edge occurs earlier than on a wing model with a supersonic leading edge. The angle of attack has a significant effect on the position of the transition point from the laminar to turbulent flow. The data presented in the article are among the first results for a swept wing with a subsonic leading edge.",
keywords = "BOUNDARY-LAYER, NUMBER",
author = "Semionov, {N. V.} and Kosinov, {A. D.} and Yermolaev, {Yu G.} and Kocharin, {V. L.} and Shipul, {S. A.} and Yatskikh, {A. A.}",
note = "Publisher Copyright: {\textcopyright} 2020 Author(s). Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 27th Conference on High-Energy Processes in Condensed Matter, HEPCM 2020 ; Conference date: 29-06-2020 Through 03-07-2020",
year = "2020",
month = oct,
day = "26",
doi = "10.1063/5.0028295",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin, {Vasily M.}",
booktitle = "High-Energy Processes in Condensed Matter, HEPCM 2020",
}