Nacelle design for ultra-high bypass ratio engines with CFD based optimisation-Reference-Cited by-同舟云学术

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Nacelle design for ultra-high bypass ratio engines with CFD based optimisation

Published:2021-06 Issue: Volume:113 Page:106191
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Robinson Matthew,MacManus David G.^ORCID,Christie Robert,Sheaf Christopher,Grech Nicholas

Funder

Engineering and Physical Sciences Research Council

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Jane's Aero-Engines,2009

2. Installation features of advanced, very high bypass turbofan propulsion systems;Marx,1989

3. Energy efficient engine program advanced turbofan nacelle definition study;Howe,1985

4. Potential improvement of aerodynamic performance by morphing the nacelle inlet;Majic;Aerosp. Sci. Technol.,2016

5. Concepts and technologies for the next generation of large civil aircraft engines;Haselbach,2014

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