Experimental determination of the range of applicability of the transonic area rule for wings of triangular plan form / William A. Page.
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 ra...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3872. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3872
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| Y 3.N 21/5:6/3872 | Available Place a Hold |