Design and analysis of non-axisymmetric installed aero-engine exhaust systems-Reference-Cited by-同舟云学术

Design and analysis of non-axisymmetric installed aero-engine exhaust systems

Published:2020-11 Issue: Volume:106 Page:106210
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Otter John J.^ORCID,Goulos Ioannis^ORCID,Christie Robert,MacManus David G.^ORCID

Funder

Rolls-Royce

Engineering and Physical Science Research Council

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

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

2. Optimum fan pressure ratio for bypass engines with separate or mixed exhaust streams;Guha;J. Propuls. Power,2001

3. Aerodynamic design of an ultra-low rotating speed geared fan;Zhang;Aerosp. Sci. Technol.,2017

4. Aerodynamic design of separate-jet exhausts for future civil aero-engines part I: parametric geometry definition and computational fluid dynamics approach;Goulos;J. Eng. Gas Turbines Power,2016

5. Aerodynamic effects of propulsion integration for high bypass ratio engines;Stankowski;J. Aircr.,2017

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Impact of Installation on the Performance of an Aero-Engine Exhaust at Wind-Milling Flow Conditions;Journal of Engineering for Gas Turbines and Power;2024-02-01

2. Design optimisation of non-axisymmetric exhausts for installed civil aero-engines;Aerospace Science and Technology;2023-11

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

4. Design considerations of non-axisymmetric exhausts for large civil aero-engines;AIAA AVIATION 2023 Forum;2023-06-08

5. Computational assessment of non-axisymmetric separate-jet exhausts on test rig configurations;AIAA AVIATION 2023 Forum;2023-06-08