Multi-objective optimisation of short nacelles for high bypass ratio engines-Reference-Cited by-同舟云学术

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Multi-objective optimisation of short nacelles for high bypass ratio engines

Published:2019-08 Issue: Volume:91 Page:410-421
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Tejero Fernando,Robinson Matthew,MacManus David G.,Sheaf Christopher

Funder

Rolls-Royce

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. 2020 vision: the prospects for large civil aircraft propulsion;Birch;Aeronaut. J.,2000

2. Preparing for the future: reducing gas turbine environmental impact – IGTI scholar lecture;Cumpsty;J. Turbomach.,2010

3. Analysis of Turbofan Propulsion System Weight and Dimensions;Waters,1977

4. Installation features of advances, very high bypass turbofan propulsion systems;Marx,1989

5. Ultra-Efficient Engine Technology Systems Integration and Environmental Assessment;Dagget,2002

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1. Comparison of Overwing and Underwing Nacelle Aeropropulsion Optimization for Subsonic Transport Aircraft;Journal of Aircraft;2023-09-05

2. A New Circular Section Control for Streamwise Profiles in Aeroengine Nacelle Cowl Design and Optimization;Journal of Aerospace Engineering;2023-09

3. Multi-fidelity and multi-objective aerodynamic short nacelle shape optimisation under different flight conditions;The Aeronautical Journal;2023-08-09

4. Over-wing integration of ultra-high bypass ratio engines: A coupled wing redesign and engine position study;Aerospace Science and Technology;2023-07

5. Propulsion integration study of civil aero-engine nacelles;The Aeronautical Journal;2023-06-13

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