A High-Output Reciprocating Engine Design
A High-Output Reciprocating Engine Design
A Proposal for Large Internal Combustion Engines Using a Two-Stroke Cycle with Crankcase Compression and Piston-Head Valves
- Neue Suche nach: Castellini, A.
- Neue Suche nach: Castellini, A.
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.
Dokumentinformationen
A High-Output Reciprocating Engine Design
A Proposal for Large Internal Combustion Engines Using a Two-Stroke Cycle with Crankcase Compression and Piston-Head Valves
Aircraft Engineering and Aerospace Technology ; 20 , 6 ; 179-181
1948-06-01
3 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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