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Thermodynamic Efficiency of Present Types of Internal Combustion Engines for AircraftReport presents requirements of internal combustion engines suitable for aircraft. Topics include: (1) service requirements for aeronautic engines - power versus weight, reliability, and adaptability factors, (2) general characteristics of present aero engines, (3) aero engine processes and functions of parts versus power-weight ratio, reliability, and adaptability factors, and (4) general arrangement, form, proportions, and materials of aero parts - power-weight ratio, reliability, and adaptability.
Document ID
19930091032
Acquisition Source
Headquarters
Document Type
Other - NACA Technical Report
Authors
Charles E Lucke
(Columbia University New York, United States)
Date Acquired
September 6, 2013
Publication Date
January 31, 1916
Publication Information
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
NACA-TR-7
Accession Number
93R20322
Distribution Limits
Public
Copyright
Public Use Permitted.
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