Single-component molecular tagging velocimetry of the boundary layer on a NACA-0012 airfoil plunging across uniform-shear flow-Reference-Cited by-同舟云学术

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Single-component molecular tagging velocimetry of the boundary layer on a NACA-0012 airfoil plunging across uniform-shear flow

Published:2020-01-05 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2020 Forum
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Author:

Albrecht Mitchell B.¹,Naguib Ahmed M.¹,Koochesfahani Manoochehr¹

Affiliation:

1. Michigan State University

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Frost, W., and Shabibi, A. M. "A Field Study of Wind Over a Simulated Block Building." NASA Report CR-2804, 1977(https://ntrs.nasa.gov/search.jsp?R=19770011713)

2. Woo H. G. C., Peterka, J. A., and Cermak, J. E. "Wind-Tunnel Measurements in the Wakes of Structures." NASA Report CR-2806, 1977(https://ntrs.nasa.gov/search.jsp?R=19770012772)

3. Review: the atmospheric boundary layer

4. An experimental study of the dynamic and steady-state flow disturbances encountered by aircraft during a carrier landing approach.

Cited by 1 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. Reynolds Number and Freestream Shear Effects on a NACA 0012 Airfoil in the Reynolds Number Range 10,000-30,000;AIAA SCITECH 2022 Forum;2022-01-03

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