Multipoint Aerodynamic Design of Ultrashort Nacelles for Ultrahigh-Bypass-Ratio Engines
Author:
Affiliation:
1. Chalmers University of Technology, 412 58 Gothenburg, Sweden
2. GKN Aerospace, 461 81 Trollhättan, Sweden
3. LFV Operations, 438 80 Landvetter, Sweden
Funder
VINNOVA - Swedish Governmental Agency for Innovation Systems
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38497
Reference43 articles.
1. An Automated Approach to Nacelle Parameterization Using Intuitive Class Shape Transformation Curves
2. The use of hybrid intuitive class shape transformation curves in aerodynamic design
3. Surrogate-based aerodynamic optimisation of compact nacelle aero-engines
4. Multi-objective optimisation of short nacelles for high bypass ratio engines
5. Aerodynamics of aero-engine installation
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