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A HighOutput Reciprocating Engine Design

A HighOutput Reciprocating Engine Design IN the development of the reciprocating aeroengine it is not often possible to announce a marked step forward in the constant endeavour to improve the important factors of b.h.p.weight ratio and economy, but it is believed that the design of the Lindum 6,5004,500 and 4,000 h.p. aeroengine which is described here represents an advance of a nature which has not been achieved for many years. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

A HighOutput Reciprocating Engine Design

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031646
Publisher site
See Article on Publisher Site

Abstract

IN the development of the reciprocating aeroengine it is not often possible to announce a marked step forward in the constant endeavour to improve the important factors of b.h.p.weight ratio and economy, but it is believed that the design of the Lindum 6,5004,500 and 4,000 h.p. aeroengine which is described here represents an advance of a nature which has not been achieved for many years.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Jun 1, 1948

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