PLIF Visualization of Active Control of Hypersonic Boundary Layers Using Blowing-Reference-Cited by-同舟云学术

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PLIF Visualization of Active Control of Hypersonic Boundary Layers Using Blowing

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
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Author:

Bathel Brett¹,Danehy Paul²,Inman Jennifer²,Alderfer David²,Berry Scott²

Affiliation:

1. University of Virginia

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4266

Reference17 articles.

1. Boundary Layer Control for Hypersonic Airbreathing Vehicles

2. Hypersonic Boundary-Layer Trip Development for Hyper-X

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1. Nitric Oxide Planar Laser Induced Fluorescence Rotational Thermometry Characterization of a Hypersonic Boundary Layer;AIAA SCITECH 2024 Forum;2024-01-04

2. Experimental investigation of boundary layer transition on a swept flat plate under variable Reynolds number;Fluid Dynamics;2022-06

3. Research Progress of hypersonic boundary layer transition control experiments;Advances in Aerodynamics;2022-04-20

4. Numerical Study of Crossflow Jet Generated Instabilities in a High-Speed Boundary Layer;IUTAM Laminar-Turbulent Transition;2021-07-31

5. Experimental Investigation of the Hypersonic Boundary Layer Transition on a 45° Swept Flat Plate;Fluid Dynamics;2020-01

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