Selecting Optimal Dimensions for a High-Temperature Aircraft Starter Generator-Reference-Cited by-同舟云学术

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Selecting Optimal Dimensions for a High-Temperature Aircraft Starter Generator

Published:2018-01 Issue:1 Volume:89 Page:21-24
ISSN:1068-3712
Container-title:Russian Electrical Engineering
language:en
Short-container-title:Russ. Electr. Engin.

Author:

Ismagilov F. R.,Ismagilov Sh. G.,Tarasov N. G.,Ayguzina V. V.

Publisher

Allerton Press

Subject

Electrical and Electronic Engineering

Link

http://link.springer.com/article/10.3103/S1068371218010078/fulltext.html

Reference2 articles.

1. Jones, R.I., The more electric aircraft: the past and the future, IEE Colloquium Electrical Machines and Systems for the More Electric Aircraft, London: Inst. Electr. Eng., 1999, pp. 1/1–1/4.

2. Besnard, J.-P., Biais, F., and Martinez, M., Electrical rotating machines and power electronics for new aircraft equipment systems, Proc. 25th Congr. of the International Council of the Aeronautical Sciences 2006, Red Hook, NY: Curran Associates, 2006.

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