Fine structures of self-sustaining dual jets in supersonic crossflow
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
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1. Trailing-edge shock loss control with self-sustaining synthetic jet in a supersonic compressor cascade;Chinese Journal of Aeronautics;2023-07
2. The Influence of Steady Air Jet on the Trailing-Edge Shock Loss in a Supersonic Compressor Cascade;Aerospace;2022-11-12
3. Effects of confinement and curvature on a jet in a supersonic cross-flow;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-04-18
4. Vortical structures and density fluctuations analysis of supersonic forward-facing step controlled by self-sustaining dual synthetic jets;Acta Mechanica Sinica;2020-11-03
5. Supersonic boundary layer transition induced by self-sustaining dual jets*;Chinese Physics B;2020-01-01
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