A High‐Power Two‐Cycle Sleeve‐Valve Engine for Aircraft: A Description of the Development of the Two‐Cycle Petrol‐Injection Research Units Built and Tested in the Laboratory of Messrs Ricardo & Co. Ltd.

Abstract

The first part of this section deals in general with considerations of engine design, and the latter part with the effects of engine operating conditions.

Citation

Hiett, G.F. and Robson, J.V.B. (1950), "A High‐Power Two‐Cycle Sleeve‐Valve Engine for Aircraft: A Description of the Development of the Two‐Cycle Petrol‐Injection Research Units Built and Tested in the Laboratory of Messrs Ricardo & Co. Ltd.", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 2, pp. 32-45. https://doi.org/10.1108/eb031858