Measurement of Boundary Layer Transition on Oscillating Airfoil using cntTSP in Low-Speed Wind Tunnel-Reference-Cited by-同舟云学术

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Measurement of Boundary Layer Transition on Oscillating Airfoil using cntTSP in Low-Speed Wind Tunnel

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

Ikami Tsubasa¹,Fujita Koji¹,Nagai Hiroki¹,Yorita Daisuke²

Affiliation:

1. Tohoku University

2. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. Evolution of a Mars Airplane Concept for the ARES Mars Scout Mission

2. Conceptual Helicopter Design for Exploration of Pit craters and Caves on Mars

Cited by 2 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. Quantification technique of transition to turbulence in boundary layers using infrared thermography;International Journal of Heat and Mass Transfer;2022-02

2. Boundary Layer Transition Measured by DIT on the PSP Rotor in Forward Flight;Journal of the American Helicopter Society;2021

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