Investigation of HL-CRM Aerodynamics With a UHBPR Nacelle in Powered-on Condition
Author:
Affiliation:
1. Technical University of Braunschweig
2. University of Padua
3. HIT09
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3547
Reference28 articles.
1. Fan Noise Reduction with Increased Bypass Nozzle Area
2. Aircraft Engine Technology for Green Aviation to Reduce Fuel Burn
3. Towards the optimum ducted UHBR engine
4. Advanced propulsion systems for large subsonic transports
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