Assessment of engine modelling on the installed aerodynamics of an ultra-high bypass turbofan
Author:
Affiliation:
1. Universita degli Studi di Padova
2. Hit09, S.r.l
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0206
Reference29 articles.
1. Civil turbofan propulsion system integration studies using powered testing techniques at ARA, Bedford
2. PAN AIR applications to aero-propulsion integration
3. Investigations of propulsion integration interference effects on a transport aircraft configuration
4. Drag Prediction of Engine-Airframe Interference Effects Using Unstructured Navier-Stokes Calculations
5. Progress in Boundary Layer Ingesting Embedded Engine Research
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