Quantitative Boundary-Layer Transition Measurements Using IR Thermography
Author:
Affiliation:
1. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1411
Reference2 articles.
Cited by 8 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. On the Use of Infrared Thermography for Boundary Layer Analysis;AIAA Scitech 2019 Forum;2019-01-06
2. IR thermography for dynamic detection of laminar-turbulent transition;Experiments in Fluids;2016-05
3. Infrared thermography for detection of laminar–turbulent transition in low-speed wind tunnel testing;Experiments in Fluids;2016-04-30
4. Effects of Step-Excrescence Location on Swept-Wing Transition;53rd AIAA Aerospace Sciences Meeting;2015-01-03
5. Flight Test Experiments on Discrete Roughness Element Technology for Laminar Flow Control;53rd AIAA Aerospace Sciences Meeting;2015-01-03
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