The B.M.W. 801 Aero‐Engine
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 August 1942
Abstract
THE B.M.W.801 is an air‐cooled, 14‐cylinder, 4‐strokc, 2‐row radial, fuel‐injection engine with reduction gear and engine‐driven cooling‐fan. Supercharging is by a single‐stage centrifugal blower with two automatic speed changes (Figs. 1 and 2).
Citation
(1942), "The B.M.W. 801 Aero‐Engine", Aircraft Engineering and Aerospace Technology, Vol. 14 No. 8, pp. 223-228. https://doi.org/10.1108/eb030930
Publisher
:MCB UP Ltd
Copyright © 1942, MCB UP Limited