Shock wave – boundary layer interaction control by wall ventilation-Reference-Cited by-同舟云学术

Shock wave – boundary layer interaction control by wall ventilation

Published:2003-04 Issue:3 Volume:7 Page:171-179
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Doerffer Piotr P.,Bohning Rainer

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference7 articles.

1. J. Ackeret, F. Feldmann, H. Rott, Untersuchung an Verdichtungstössen und Grenzschichten in schnell bewegten Gasen, Bericht No. 10 des Institutes für Aerodynamik, ETH Zürich, 1946

2. J. Delery, J.G. Marvin, Shock-wave boundary layer interactions, AGARD-AG-280, 1985

3. Shock-induced separation and its prevention by design and boundary layer control;Pearcey,1961

4. E. Stanewsky, Shock boundary layer interaction, AGARD-AR-224, 1988

5. Community research in Aerodynamics, European Commission, Directorate General XII, Science, Research and Development,1999

Cited by 24 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Correlations between thermodynamic fluctuations in shock wave/turbulent boundary layer interaction;Physical Review Fluids;2024-07-31

2. Comprehensive assessments of hypersonic inlet restart using active jet;AIAA AVIATION 2023 Forum;2023-06-08

3. The efficiency of transpiration flow through perforated plate;Aerospace Science and Technology;2021-03

4. On the Importance of Transition Control at Transonic Compressor Blades;Journal of Turbomachinery;2021-03-01

5. Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows;Acta Astronautica;2020-09