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The effect of compression ratio, cooled exhaust gas mixed with inlet air, and inlet-air temperature on the knock-limited performance of a full-scale single-cylinder engine
- Author / Creator
- Available as
- Online
- Summary
-
The object of this report was to determine the effect on the knock-limited permissible power out-put, on the specific indicated specific fuel consumption, and on the cylinder temperatures (1) of ex...
The object of this report was to determine the effect on the knock-limited permissible power out-put, on the specific indicated specific fuel consumption, and on the cylinder temperatures (1) of exhaust-gas dilution of the inlet-air charge, (2) of inlet-air temperature without exhaust-gas dilution, and (3) of compression ratio.
Details
- Creator
- by Ray E. Bolz and Roland Breitwieser
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1944
- Physical Details
-
- 1 online resource (16, [19] pages) : illustrations, tables
- data file
- OCLC
- on1411005835
- Title from title screen (viewed November 29, 2023)
- Date of issue: March 1944.
- NACA Wartime Report E-124.
- Originally issued as NACA as Advance Restricted Report 4C31.
- Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.
- Includes bibliographical references (page 16)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.