Design considerations of non-axisymmetric exhausts for large civil aero-engines
Author:
Affiliation:
1. Cranfield University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3467
Reference42 articles.
1. 2020 vision: the prospects for large civil aircraft propulsion
2. Civil turbofan propulsion aerodynamics: Thrust-drag accounting and impact of engine installation position
3. Otter, J. J. "Aerodynamics and Performance of Civil Aero-Engine Exhaust Systems," PhD Thesis,Cranfield University, Cranfield, Bedfordshire, UK, 2018.
4. Parametric design of non-axisymmetric separate-jet aero-engine exhaust systems
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