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Answers |
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A straight line at less than a 45o angle through 0,0. The lift and angle show + and - numbers. |
The straight line shows a steady increase. If you double the angle, then you double the lift. |
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A slight upward curve. |
The curve shows that as the thickness increases the lift also increases, but to a lesser degree. |
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At angle = 0.0, there is no line on the graph. |
For a symmetric airfoil, a change in thickness will not change the lift. |
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A straight line at less than a 45o angle through 0,0 with lift being both + and -. |
The straight line shows a steady increase.
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An upward curve where the slope of the line increases with increased speed. |
The upward curve shows that lift increases at a greater rate than the speed increases. |
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At angle = 0.0, there is no line. |
For a symmetric airfoil, a change in airspeed does not create lift. |
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A downward curving line where the slope decreases with altitude. |
As altitude increases the lift that results decreases; but the decrease lessens with altitude. ( As the altitude increases, the density of the air decreases. So lift decreases as density decreases.) |
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A straight line at a 45o angle through 0,0. |
The lift increases at the same rate as the area. |
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