Impact of installation on a civil large turbofan exhaust system at idle descent conditions-Reference-Cited by-同舟云学术

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Impact of installation on a civil large turbofan exhaust system at idle descent conditions

Published:2021-12 Issue: Volume:119 Page:107125
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Rao Anirudh N.^ORCID,Goulos Ioannis^ORCID,MacManus David G.^ORCID

Funder

European Commission

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference67 articles.

1. Benefits of continuous descent operations in high-density terminal airspace considering scheduling constraints;Robinson,2010

2. Evaluation of fuel benefits depending on continuous descent approach procedures;Cao;Air Traffic Control Q.,2014

3. Predictability, variability and operational feasibility aspect of CDA;Pradeep,2017

4. Advanced methods for propulsion system integration in aircraft conceptual design;Seitz,2012

5. Gas Turbine Performance;Walsh,2004

Cited by 3 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. Coupled propulsive and aerodynamic analysis of an installed ultra-high bypass ratio powerplant at high-speed and high-lift conditions;AIAA AVIATION 2023 Forum;2023-06-08

3. Predicting the energy and exergy performance of F135 PW100 turbofan engine via deep learning approach;Energy Conversion and Management;2022-08

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