Horizontal tail loads in maneuvering flight /
A method is derived for determining the horizontal tail load following a prescribed maneuver. The tail load is broken down into various components which are examined to determine the maximum values. The method is extended to include suggestions for distributing the load across the span as well as in...
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| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2078 |
| Subjects: | |
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| Call Number: |
NACA TN 2078 |
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