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Comparison of calculated and experimental propeller characteristics for four-, six-, and eight-blade single-rotating propellers
- Author / Creator
- Available as
- Online
- Summary
-
The calculated performance of four-, six-, and eight-blade single-rotating propellers has been compared with experimental results for blade angles ranging from 25 to 65 degrees. The experimental da...
The calculated performance of four-, six-, and eight-blade single-rotating propellers has been compared with experimental results for blade angles ranging from 25 to 65 degrees. The experimental data were obtained on propellers mounted in front of a streamline body with a spinner housing the hub. The calculated propeller performance was found to be in good agreement with the experimental results over the complete range of blade angle investigated. The method of calculations is presented in detail and a sample computation is included.
Details
- Creator
- by John L. Crigler
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1944
- Physical Details
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- 1 online resource (10, [19] pages) : illustrations, table
- data file
- OCLC
- on1431128747
- Title from title screen (viewed April 24, 2024)
- Date of issue: February 1944.
- NACA Wartime Report L-362.
- Originally issued as NACA as Advance Confidential Report L4A04.
- Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
- Includes bibliographical references (page 9)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.