Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels-Reference-Cited by-同舟云学术

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Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels

Published:2012 Issue: Volume: Page:
ISSN:
Container-title:Progress in Flight Physics
language:
Short-container-title:

Author:

Borovoy V.,Mosharov V.,Noev A.,Radchenko V.

Publisher

EDP Sciences

Link

http://www.eucass-proceedings.eu/10.1051/eucass/201203015/pdf

Cited by 13 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. Investigation on transition correlation of conical boundary layer in hypersonic wind tunnel experiments;Acta Astronautica;2022-12

2. Heat flow measurements on high-speed aircraft models;IOP Conference Series: Materials Science and Engineering;2020-09-01

3. Effect of Görtler-like vortices of various intensity on heat transfer in supersonic compression corner flows;International Journal of Heat and Mass Transfer;2020-04

4. Entropy Effect in Laminar-Turbulent Transition of the Supersonic Boundary Layer in the Wake of an Isolated Roughness;Fluid Dynamics;2020-01

5. Heat Transfer Determined by the Temperature Sensitive Paint Method;Transactions on Aerospace Research;2018-12-01

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