Evaluation of a fixed spoiler as a gust alleviator /
The results of an investigation made in the Langley gust tunnel to determine the effectiveness of a fixed spoiler as a gust alleviator show that approximately the same maximum acceleration is experienced by the model with or without the spoiler in a sharp-edge gust. In a gust with a gradient distanc...
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1948
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1753 |
| Subjects: | |
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| Call Number: |
NACA TN 1753 |
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