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- W1956316706 abstract "IN the development of the reciprocating aero‐engine it is not often possible to announce a marked step forward in the constant endeavour to improve the important factors of b.h.p./weight ratio and economy, but it is believed that the design of the Lindum 6,500–4,500 and 4,000 h.p. aero‐engine which is described here represents an advance of a nature which has not been achieved for many years." @default.
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- W1956316706 date "1948-06-01" @default.
- W1956316706 modified "2023-09-26" @default.
- W1956316706 title "A High‐Output Reciprocating Engine Design" @default.
- W1956316706 doi "https://doi.org/10.1108/eb031646" @default.
- W1956316706 hasPublicationYear "1948" @default.
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