High-Speed PIV Applied to Wake of NASA CRM Model in ETW Under High Re-Number Stall Conditions for Sub- and Transonic Speeds-Reference-Cited by-同舟云学术

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High-Speed PIV Applied to Wake of NASA CRM Model in ETW Under High Re-Number Stall Conditions for Sub- and Transonic Speeds

Published:2015-01-03 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA Aerospace Sciences Meeting
language:
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Author:

Konrath Robert¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1095

Reference7 articles.

Cited by 12 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. Capturing Unsteady Flow Phenomena at High Speed Stall Conditions by Adaptation and Application of Cryogenic PIV;AIAA SCITECH 2024 Forum;2024-01-04

2. Numerical Investigation of Stall Characteristics of Common Research Model Configuration Based on Zonal Detached Eddy Simulation Method;Aerospace;2023-09-18

3. Application of femtosecond-laser tagging for unseeded velocimetry in a large-scale transonic cryogenic wind tunnel;Experiments in Fluids;2021-04-17

4. A review of installation effects of ultra-high bypass ratio engines;Progress in Aerospace Sciences;2020-11

5. Unseeded velocimetry in nitrogen for high-pressure, cryogenic wind tunnels: part III. Resonant femtosecond-laser tagging;Measurement Science and Technology;2020-04-29

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