Plasma-Actuated Flow Control of Hypersonic Crossflow-Induced Boundary-Layer Transition in a Mach-6 Quiet Tunnel-Reference-Cited by-同舟云学术

Plasma-Actuated Flow Control of Hypersonic Crossflow-Induced Boundary-Layer Transition in a Mach-6 Quiet Tunnel

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Yates Harrison¹,Juliano Thomas J.¹,Matlis Eric H.¹,Tufts Matthew W.²

Affiliation:

1. University of Notre Dame

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1076

Reference21 articles.

1. 2Ward, C. A. C., Crossflow Instability and Transition on a Circular Cone at Angle of Attack in a Mach-6 Quiet Tunnel, Ph.D. thesis,Purdue University, 2014.

2. 3Schuele, C. Y., Control of Stationary Crossflow Modes Using Stationary Patterned Roughness and DBD Plasma Actuators at Mach 3.5, Ph.D. thesis,University of Notre Dame, 2011.

3. Analysis of Instabilities in Non-Axisymmetric Hypersonic Boundary Layers over Cones

4. Hypersonic Lifting Body Windward Surface Flow-Field Analysis for High Angles of Incidence

Cited by 10 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. Boundary layer transition of hypersonic flow over a delta wing;Journal of Fluid Mechanics;2024-02-10

2. Schlieren Visualization of Controlled Disturbances in Mach 5 Flow Over a Hollow Cylinder Flare;AIAA SCITECH 2023 Forum;2023-01-19

3. Effect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer Transition;AIAA Journal;2022-12

4. Experimental study on surface arc plasma actuation-based hypersonic boundary layer transition flow control;Plasma Science and Technology;2022-07-20

5. Development of Plasma-based Controlled Disturbances for the Study of Boundary Layer Transition and Shock Boundary Layer Interaction;AIAA AVIATION 2021 FORUM;2021-07-28