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Thomas Borchert writes:
Frankly, I have never quite understood the distinction, same as with "forward" and "side" slips. My reasoning is that all lift in the aircraft is the result of it moving through air, which in turn is caused by thrust from the powerplant. Therefore there should be a strong relationship between thrust (power) and altitude, if the aircraft is not specifically trimmed to change it. And if the aircraft is trimmed to change it, then lift will be traded for forward airspeed. Thus, setting the throttles high will produce more lift and raise the airplane to a higher altitude. If the aircraft is trimmed to maintain level flight with that power, it will accelerate forward, trading lift for forward momentum. In contrast, if the pitch is changed alone, it simply shifts any existing momentum from one dimension to another. If you pitch downward, lift is traded for forward speed. If you pitch upward, speed is traded for lift. But the sum of both has to remain the same; the only way to change the overall sum is with adjustments to power. This also means that, if pitch is trimmed to hold it constant, more power means more speed, and less power means less speed. Taking this further, most control movements convert kinetic dimension in one dimension into kinetic energy in another dimension, but total kinetic energy must remain constant. An exception is control movements that create only drag, which convert kinetic energy to heat and reduce total energy remaining in the aircraft. To add energy, you have to use the powerplant. In the case of gliders, they are limited to whatever kinetic energy they start with. However, since they are light, if they can find rising columns of air, they can extract energy from these columns and convert it to lift and/or airspeed. As long as they can find rising air, they can remain aloft indefinitely. The same is true for vultures. -- Transpose mxsmanic and gmail to reach me by e-mail. |
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