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THE information available on the performance characteristics of high‐speed, compression‐ignition engines has usually been published as results of tests of particular engines, and these results have been judged entirely on a basis of brake horse‐power and specific fuel consumption. Much more detailed information is necessary for a foundation upon which to base further development so that the inherent advantages of this type of engine may be generally used in aerial transportation.
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© MCB UP Limited
1931
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