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Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel
- Author / Creator
- Available as
- Online
- Summary
-
An investigation to determine the effects of wing loading and altitude on lateral stability and control has been carried out in the NACA free-flight tunnel. The results of the flight tests of the m...
An investigation to determine the effects of wing loading and altitude on lateral stability and control has been carried out in the NACA free-flight tunnel. The results of the flight tests of the model were correlated with calculated stability boundaries, and an effort was made to determine for each loading condition the airplane configuration that gave the best flight characteristics.
Details
- Creator
- by John P. Campbell and Charles L. Seacord, Jr
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1943
- Physical Details
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- 1 online resource (14, [7] pages) : illustrations, tables
- data file
- OCLC
- on1444262551
- Title from title screen (viewed July 9, 2024)
- Date of issue: June 1943.
- NACA Wartime Report L-522.
- Originally issued as NACA as Advance Restricted Report L3F25.
- Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
- 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.