Modelling of cryogenic cooling system design concepts for superconducting aircraft propulsion-Reference-Cited by-同舟云学术

Modelling of cryogenic cooling system design concepts for superconducting aircraft propulsion

Published:2016-09 Issue:3 Volume:6 Page:170-178
ISSN:2042-9738
Container-title:IET Electrical Systems in Transportation
language:en
Short-container-title:IET Electrical Systems in Transportation

Author:

Palmer Joseph¹,Shehab Essam¹

Affiliation:

1. Department of ManufacturingSchool of Aerospace, Transport and ManufacturingCranfield UniversityCranfieldMK43 0ALBedfordshireUK

Funder

Engineering and Physical Sciences Research Council

Cranfield University

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-est.2015.0020

Reference21 articles.

1. Challenges of future aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric commercial aircraft

2. European Commission Directorate‐General for Research and Innovation: ‘Flightpath 2050: Europe's goal for aviation’ 2011 doi:https://doi.org/10.2777/50266

3. Airbus Group Innovations: ‘Airbus E‐Thrust Concept Images’. Available athttp://www.airbusgroup.com/int/en/news‐media/media~item=ae86b8b3‐fe93–45a7‐b3b5‐ca5a6214f348~.html accessed 15 January 2015

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