NASA NTRS ยท 19930094849
Development of the Junkers-diesel Aircraft Engine
Abstract
The working process of the Junkers engine has resulted from a series of attempts to attain high performance and to control the necessarily rapid and complete combustion at extremely high speeds. The two main problems of Diesel engines in aircraft are addressed; namely, incomplete combustion and the greater weight of Diesel engine parts compared to gasoline engines.
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Gasterstadt,. 1930-05-01. Development of the Junkers-diesel Aircraft Engine. https://ntrs.nasa.gov/citations/19930094849
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