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

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Appendix B: Sizing Results<br />

Appendix B: Sizing Results<br />

Relative Lifting Capacity (kg)<br />

2.1<br />

1.9<br />

1.7<br />

1.5<br />

1.3<br />

1.1<br />

0.9<br />

0.7<br />

600 W, 0.4 m<br />

800 W, 0.4 m<br />

1000 W, 0.4 m<br />

600 W, 0.5 m<br />

800 W, 0.5 m<br />

1000 W, 0.5 m<br />

600 W, 0.6 m<br />

800 W, 0.6 m<br />

1000 W, 0.6 m<br />

0.5<br />

0 10 20 30 40 50 60 70 80 90 100<br />

Flap Angle (degrees)<br />

Figure B-1: Relative Lifting Capacity <strong>for</strong> Various Engine Powers and Wing<br />

Lengths at 15 m/s Flight Speed<br />

80<br />

70<br />

Wing Length 0.3 m<br />

Flapping Frequency (Hz)<br />

60<br />

50<br />

40<br />

30<br />

20<br />

35°<br />

45°<br />

55°<br />

65°<br />

75°<br />

85°<br />

10<br />

0<br />

100 1000 10000 100000<br />

Power Consumption (W)<br />

Figure B-2: Flapping Frequency vs. Power Consumption (Watts) <strong>for</strong> a<br />

Wing Length of 0.3 m<br />

B-1

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