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Determination of ram-jet combustion-chamber temperature by means of total-pressure surveys
- Author / Creator
- Available as
- Online
- Summary
-
A method is described by which the total temperature of the gases at the combustion-chamber outlet of a ram-jet engine may be determined from the loss in total pressure measured across the combusti...
A method is described by which the total temperature of the gases at the combustion-chamber outlet of a ram-jet engine may be determined from the loss in total pressure measured across the combustion chamber. A working chart is presented by means of which the ratio of the total temperature of the gasesat the combustion-chamber outlet to the total temperature of the gases at the combustion-chamber inlet may be determined from the measured loss of total pressure across the combustion chamber and the known values of air flow, total pressure, and total temperature at the combustion-chamber inlet.
Details
- Creator
- by I. Irving Pinkel
- Included Title
-
- Technical Report Archive & Image Library (TRAIL)
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1951
- Physical Details
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- 1 online resource (10, [1] pages) : illustrations, tables
- data file
- OCLC
- on1343851018
- "Lewis Flight Propulsion Laboratory."
- Title from title screen (viewed August 31, 2022)
- Date of issue: December 1951.
- Report numbers NACA-TN-2526.
- Includes bibliographical references (page 7)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.