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Experimental determination of the range of applicability of the transonic area rule for wings of triangular plan form
- Author / Creator
- Available as
- Online
- Summary
-
Experimental measurements have been made of the zero-lift drag rise at transonic speeds of a family of triangular plan form wings of varying thickness and aspect ratio mounted on a cylindrical body...
Experimental measurements have been made of the zero-lift drag rise at transonic speeds of a family of triangular plan form wings of varying thickness and aspect ratio mounted on a cylindrical body. Together with the transonic similarity parameters, the results of the tests are used to define the range of applicability of the transonic area rule for wings of triangular plan form. The significance of the test results is discussed.
Details
- Creator
- by William A. Page
- Format
- Books
- Language
- English
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1956
- Physical Details
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- 1 online resource (22 pages) : illustrations, photographs
- data file
- OCLC
- on1396170208
- Date of issue: December 1956.
- Report numbers NACA-TN-3872.
- "Ames Aeronautical Laboratory."
- Title from title screen (viewed July 31, 2023)
- Includes bibliographical references (page 11)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.