Assessment of Fan/Airframe aerodynamic performance using 360° uRANS computations: Code-to-Code comparison between ONERA, DLR, NLR and Airbus.-Reference-Cited by-同舟云学术

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Assessment of Fan/Airframe aerodynamic performance using 360° uRANS computations: Code-to-Code comparison between ONERA, DLR, NLR and Airbus.

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
language:
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Author:

Meheut Michael¹,Sartor Fulvio¹,Vergez Maxime¹,Laban Martin²,Schnell Rainer³,Stuermer Arne W.³,Lefevre Guillaume⁴

Affiliation:

1. ONERA

2. Netherlands Aerospace Center (NLR)

3. German Aerospace Center (DLR)

4. Airbus

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0582

Reference31 articles.

1. The Simulation of Turbomachinery Blade Rows in Asymmetric Flow Using Actuator Disks

2. Hall, D. K. "Analysis of civil aircraft propulsors with boundary layer ingestion", Ph.D. thesis,Massachusetts Institute of Technology, 2015.

3. Thollet, W. "Body-Force modeling of fan-airframe interactions", Ph.D. thesis,ISAE - Supaéro, 2017.

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