Some wind-tunnel experiments on single-degree-of-freedom flutter of ailerons in the high subsonic speed range /
Results of wind-tunnel tests of three wing models with various aileron configurations are presented. Density in the range of 0.0008 to 0.0058 slug per cubic foot has little effect on the initial amplitude or initial Mach number associated with the aileron oscillations (buzz). However, the frequencie...
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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) ;
3687 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 3687 |
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