Brief resume of development of Rolls-Royce Kestrel engine and analysis of requirements of high-performance engine of future, developing at least 1500 bhp and operating on fuels of high knock ratings; problems investigated include those of engine forms, fuels, detonation, waste-heat disposal, cooling drag, cooling medium, and mechanical and operational features; conclusions deduced. (See also - n 1 July 1936 p 267-86 (discussion) 286-7; Aeroplane v 51 n 1313 July 22 1936 p 123-6)
Liquid-cooled aero engines
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 39 , n 4
1936
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1936
|SAE Technical Papers | 1936
|Radial air-cooled aero engines
Engineering Index Backfile | 1924
|British water-cooled aero engines
Engineering Index Backfile | 1930
|British Water-Cooled Aero Engines
Emerald Group Publishing | 1929
|