Three German Engine Fuel Systems
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 October 1943
Abstract
BMW 801A/1 The engine is a radial, air‐cooled, fourteen‐cylindcr, double‐bank motor of 42 litres capacity, 6–5/1 compression ratio and 156 mm. bore and stroke.
Citation
(1943), "Three German Engine Fuel Systems", Aircraft Engineering and Aerospace Technology, Vol. 15 No. 10, pp. 293-302. https://doi.org/10.1108/eb031063
Publisher
:MCB UP Ltd
Copyright © 1943, MCB UP Limited