Shell Aviation News n 254 Aug 1959 p 14-18. Technical considerations involved in determination of 250-hp engine design, developed by General Motors for small helicopters and light military aircraft; unique features are reviewed such as free turbine, selection of engine pressure ratio and turbine inlet temperature, engine air flow, matching of components, selection of compressor configuration, control system, and mechanical configuration. (see also abstract in SAE -- J v 67 n 7 July 1959 p 54-6)
Design approach to Allison model 250 engine
SAE -- Paper
SAE Meeting ; 1959 Allison
1959
26 pages
Conference paper
English
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Design approach to Allison model 250 engine
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