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Effects of propeller operation and angle of yaw on the distribution of the load on the horizontal tail surface of a typical pursuit airplane
- Author / Creator
- Available as
- Online
- Summary
-
Measurements were made in the NACA full-scale tunnel of the pressure distribution over the horizontal tail surface of a typical pursuit airplane in order to determine the effects of propeller opera...
Measurements were made in the NACA full-scale tunnel of the pressure distribution over the horizontal tail surface of a typical pursuit airplane in order to determine the effects of propeller operation and angle of yaw on the tail load distribution. Most of the tests were made with the propeller operating to simulate climb conditions, high-speed dives, and pull-ups to various normal accelerations for angles of yaw ranging from 10 degrees to -10 degrees. Measurements were also made of the distributions of downwash angle and dynamic pressure in front of the horizontal tail and results have been correlated with the results of the pressure-distribution tests.
Details
- Creator
- by Harold H. Sweberg and Richard C. Dingeldein
- 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 (16, [43] pages) : illustrations, tables, photograph
- data file
- OCLC
- on1419831090
- Title from title screen (viewed February 2, 2024)
- NACA Wartime Report L-227.
- Originally issued as NACA as Advance Restricted Report L4B10.
- Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
- Date of issue: February 1944.
- Includes bibliographical references (page 13)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.