A Wind Tunnel Rig to Study the External Fan Cowl Separation Experienced by Compact Nacelles in Windmilling Scenarios-Reference-Cited by-同舟云学术

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A Wind Tunnel Rig to Study the External Fan Cowl Separation Experienced by Compact Nacelles in Windmilling Scenarios

Published:2023-01-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2023 Forum
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Author:

Sabnis Kshitij¹,Boscagli Luca²,Swarthout Avery²,Tejero Embuena Fernando²,Babinsky Holger¹,David MacManus²,Sheaf Christopher³

Affiliation:

1. University of Cambridge

2. Cranfield University

3. Rolls-Royce plc

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1942

Reference28 articles.

1. Commission, E. "FlightPath 2050: Europe's vision for aviation," Tech. Rep. EUR 098 EN, Publications Office of theEuropean Union, 2011.

2. Hughes, C. "The promise and challenges of ultra high bypass ratio engine technology and integration," Tech. Rep. HQ-STI-11-012, National Aeronautics and Space Administration, 2011.

3. A review of installation effects of ultra-high bypass ratio engines

4. Nacelle design for ultra-high bypass ratio engines with CFD based optimisation

5. Effect of Reynolds number on upper cowl flow separation

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. Infrared thermography techniques for boundary layer state visualisation;Experiments in Fluids;2024-06

2. Characteristics of Shock-Induced Boundary-Layer Separation on Nacelles Under Windmilling Diversion Conditions;AIAA Journal;2024-01

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