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#91
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I have no pilot training so I am interested in how pilots calculate derating factors for forces acting on, or applied by, an airstream. You did it for my buggy model but I am having trouble applying the same principle to an airplane. I understand this is an area where pilots have a lot of training and knowledge. |
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#92
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To be honest I have never heard anything so absurd as having to derate a force because it is acting on an airstream. A force is a force. It has nothing to do with what it is acting on. If a plane propeller is producing 2000N it is always 2000N. Exactly the same with my buggy 9N is 9N. It does not magically need to increase because it is acting on an airstream. Why did it not have to increase in the earlier examples where it is also acting on the airstream? Also how can 1N reduce to 0.25N because it is being applied by air. You are so convinced that it cannot work that you are coming up with stupid calculations. Go back and review what you have written. You will see it is utter stupidity. |
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#93
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| Actually, I did go back and review. And I believe I have solved problem with the forces and energies not balancing. I did make an error with the 33N of thrust. But that doesn't get the cart out of trouble with energy. Let me ask a couple questions: * How much energy is the cart demanding? Are we still in agreement that it's 33W? (Actually, it's 36W. The windage should be multiplied by 4m/s like it originally was. Not 1m/s. Another minor mistake.) * Were is the energy coming from? |
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#94
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Now you're approaching my level of frustration. Inet. Let me ask you a serious question. Are you open minded enough to believe this cart may be doing exactly what it appears to be doing? If so, we have all the time in the world to explain how it can and does do that. If not, no worries. We won't burden you with facts. Gratuitous 2nd question: do you believe that ice-boats can achieve and maintain a downwind velocity component of 3X to 4X the wind speed? |
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#95
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Regarding the problem at hand, as I've pointed out the numbers presented aren't adding up which means there's a flaw in the proposed model. Once I had a chance to get some sleep and revisit the problem, I was able for see what's going on. As was pointed out earlier, the cart in the example requires 36W of power to meet the demands of driving the prop and overcoming the other drag factors. The wind is providing 27W under the given conditions which means there's an energy shortfall. That's a problem. As it turns out, once you resolve the energy discrepancy, you'll find that you can theoretically exceed wind speed and meet the the demands of conservation of energy and balanced forces. (The maximum speed works out to be twice the wind speed.) However, it requires that the prop have 100% efficiency and that the cart have zero drag. That's not likely to happen. The equations suggest that you can achieve a fraction over wind speed with some drag and prop losses. However, the drag budget is pretty small. It would be difficult to achieve in practice. |
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#96
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I'm really curious to know why you trust your flawed analyses over real world results. |
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#97
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#98
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#99
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I have been trying to get IRK to explain the force derating factor that applies to a force that happens to be acting on an airstream. It seems to change with different conditions of velocity. Did you get to the force derating lecture during your pilots training course? If you have the lecture notes I would like to see them. I am just an ignorant electrical engineer not versed in all those key aspects of physics that enable an airplane to fly. Maybe if I could just grasp the force derating factor for a force acting on an airstream I would have a better understanding of how planes fly. |
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#100
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#101
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| The energy literally comes out of the air. The ground speed of the undisturbed airflow is 3m/s. After the vehicle passes there will be a cylindrical airstream immediately behind the cart prop that has been slowed down. Over time this will gradually be entrained into the general environment as happens with any propeller or wing. Let me provide some actual numbers. The prop has an apparent wind of 1m/s. The airflow is being accelerated as it passes through the prop. In my particular example the airflow reaches 1.28m/s. The mass flow rate to achieve my nominated prop efficiency with thrust of 9N is calculated as 44kg/s. So in this case the far field velocity for the prop is 1m/s and the near field is 1.28m/s. When the cart is doing 4m/s ground speed the far field velocity with respect to the ground is 3m/s and the near field velocity in the vicinity of the prop is 2.72m/s. The kinetic energy reduction in the propeller airstream due to the cart passing can be determined as: Energy/sec = 0.5 x 44 x (3^2 - 2.72^2) = 36W. I have done some rounding here but it shows where the energy comes from. If you set up a smoke trail you would see the air speed over the ground is slowed down in the vicinity of the prop as the cart passes by. This energy goes into overcoming the losses in the cart. Rick W |
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#102
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| Present a general set of equations describing your device. |
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#103
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| There are two papers that Mark Drela produced that I included at post #3 on this thread that gives the generalised equations of motion and energy balance. These are actually for a boat using a water turbine to power the prop. To apply them to the buggy situation you need to equate his turbine and transmission efficiency to my generator efficiency. Other than this the boat and buggy have the same generalised set of equations. I expect as you are a pilot and all you will at least know of Mark Drela. |
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#104
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#105
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| A wind tunnel test will show you guys where you went wrong in your equations. Sorry to drag up an old thread....couldn't resist |
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