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Phase II Final Report - NASA's Institute for Advanced Concepts

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Chapter 3.0 Vehicle Design<br />

3.2 Wing Motion and Structure Analysis<br />

1<br />

0 0.01 0.02 0.03 0.04 0.05 0.06<br />

0.1<br />

Wing Tip Deflection (m)<br />

Wing Section Mass (kg)<br />

0.01<br />

0.001<br />

Wing Root Thickness (m)<br />

Figure 3-23: Effect of Wing-root Thickness on Wing-tip Deflection & Wing-section Mass<br />

0.018<br />

0.3<br />

0.017<br />

Wing Tip Deflection (m)<br />

Wing Section Mass (kg)<br />

0.28<br />

0.016<br />

0.26<br />

0.015<br />

0.24<br />

0.014<br />

0.22<br />

0.013<br />

0.2<br />

0.012<br />

0.002 0.004 0.006 0.008 0.01 0.012 0.014 0.016<br />

Wing Tip Thickness (m)<br />

0.18<br />

Figure 3-24: Effect of Wing-tip Thickness on Wing-tip Deflection & Wing-section Mass<br />

63

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