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Volume 14, Issue 8
1 August 1942
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 14, Issue 8
Review Article| August 01 1942

The B.M.W. 801 Aero‐Engine

Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1942
Aircraft Engineering (1942) 14 (8): 223–228.
https://doi.org/10.1108/eb030930

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).

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© MCB UP Limited
1942
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