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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
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Article
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Tab 3
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Research Article
Efficient Method for Aeroelastic Tailoring of Composite Wing to Minimize Gust Response
Table 3
Accuracy and computation time saving of the Q-static method in different gust frequencies.
Gust frequency
0.75 Hz
1.0 Hz
1.25 Hz
1.50 Hz
Accuracy reduction
1.1%
1.5%
2.1%
2.0%
Total cycles
100
100
100
100
Time reduced by
~90%
~90%
~90%
~90%