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#261
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Stealth Pilot wrote:
On Tue, 20 May 2008 19:00:25 -0700 (PDT), More_Flaps wrote: On May 21, 12:56 am, Stealth Pilot wrote: you need to learn about somatogravic thresholds, the effect of alcohol on the viscosity of the fluids of the inner ear How much alcohol are we talking about here? Dies the viscosity of the endolymph actually change? Cheers yes. you can be quite sober and still have the viscosity reduction active in your ears some 48 hours or more later. never, never, never drink alcohol in the week before flying IFR. I'm wondering why the airlines, FAA and the military don't seem to be particularly concerned about this.... |
#262
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Gezellig was thinking very hard :
On Tue, 20 May 2008 21:00:11 +0800, Stealth Pilot wrote: On Sun, 18 May 2008 23:46:31 -0400, Gezellig wrote: Being primarily creatures earthbound (land underfoot), where feelings are our primary sources of instrument accuracy (speed in a car, wind in our hair), its kewl to trust those sensory inputs. A lot of day-in/day-out experiences too. so totally incompetent a viewpoint that you are stunning. I see. Because I interact in a thread, and am newer at piloting than you, you get to act like an asshole and treat me with high disdain. This embellishes your ego, strikes you in a positive way, makes your life happy as a clam. I, because of my age and newness, am incompetent. I must wait until I am as bright as you, hunt Usenet like a jaguar and pounce on newbies, again, emulating you and acting like an asshole. I wasn't aware of the privileges of experience. I can hardly wait. to become the next BunnyIP, Bendover or StealthSockPuppet pilot. In the meantime, let me practice. Outside of piloting data, is there anything except rocks and pebbles in your cranium? To elaborate, my suggestion is that before posting you should give your head a shake to determine if there is anything inside and to consider whether you really wished to make the fact public. Gee, I feel like IFRed already. wow LOL You go G. lol |
#263
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On May 21, 12:56 pm, Mxsmanic wrote:
Stealth Pilot writes: aeroplanes fly because of lift generated by pressure differences on the wing surfaces. Airplanes fly because the wings divert the air through which they pass downwards, creating a downwash and exerting a force in doing so that engenders an opposite force that is lift. ... these pressure differences are caused by the shape of the aerofoil of the wing ... The air is diverted because the wing has a positve angle of attack. It can be perfectly flat and it will still generate lift. So you're saying the sky does suck after all? What about rocket propulsion in a vacuum? How does that work? |
#264
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On Wed, 21 May 2008 19:56:35 +0200, Mxsmanic
wrote: Stealth Pilot writes: aeroplanes fly because of lift generated by pressure differences on the wing surfaces. Airplanes fly because the wings divert the air through which they pass downwards, creating a downwash and exerting a force in doing so that engenders an opposite force that is lift. ... these pressure differences are caused by the shape of the aerofoil of the wing ... The air is diverted because the wing has a positve angle of attack. It can be perfectly flat and it will still generate lift. downwash occurs after the wing has passed. how does it transmit its effect to the wing? magnetism? |
#265
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Mxsmanic wrote:
Stealth Pilot writes: aeroplanes fly because of lift generated by pressure differences on the wing surfaces. Airplanes fly because the wings divert the air through which they pass downwards, creating a downwash and exerting a force in doing so that engenders an opposite force that is lift. ... these pressure differences are caused by the shape of the aerofoil of the wing ... The air is diverted because the wing has a positve angle of attack. It can be perfectly flat and it will still generate lift. If that were the case a 747 would have to be producing over 250,000 pounds of force straight down. Why then am I not crushed when a 747 flies over me? |
#266
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On May 21, 12:56 pm, Mxsmanic wrote:
Stealth Pilot writes: aeroplanes fly because of lift generated by pressure differences on the wing surfaces. Airplanes fly because the wings divert the air through which they pass downwards, creating a downwash and exerting a force in doing so that engenders an opposite force that is lift. ... these pressure differences are caused by the shape of the aerofoil of the wing ... The air is diverted because the wing has a positve angle of attack. It can be perfectly flat and it will still generate lift. There is an interesting article in Flying magazine by Peter Garrison that talks about lift theory. I thought that one of the most interesting points he made was that the lift force generated by an airfoil is greater at the optimum angle of attack than would be the force imparted to it if you were to move it through the air perpendicular to the air flow at the same speed. I agree that a flat wing will produce lift at a positive AOA even without an airfoil shape - it just won't be as efficient as it would otherwise be if it were shaped like an airfoil, and talk about pitch divergent... Oh yeah, the article also pretty much discounts Bernoulli as having anything to do with why a wing produces lift. BDS |
#267
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BDS wrote:
On May 21, 12:56 pm, Mxsmanic wrote: Stealth Pilot writes: aeroplanes fly because of lift generated by pressure differences on the wing surfaces. Airplanes fly because the wings divert the air through which they pass downwards, creating a downwash and exerting a force in doing so that engenders an opposite force that is lift. ... these pressure differences are caused by the shape of the aerofoil of the wing ... The air is diverted because the wing has a positve angle of attack. It can be perfectly flat and it will still generate lift. There is an interesting article in Flying magazine by Peter Garrison that talks about lift theory. I thought that one of the most interesting points he made was that the lift force generated by an airfoil is greater at the optimum angle of attack than would be the force imparted to it if you were to move it through the air perpendicular to the air flow at the same speed. I agree that a flat wing will produce lift at a positive AOA even without an airfoil shape - it just won't be as efficient as it would otherwise be if it were shaped like an airfoil, and talk about pitch divergent... Oh yeah, the article also pretty much discounts Bernoulli as having anything to do with why a wing produces lift. BDS Any article that "discounts Bernoulli" as having anything to do with lift is incorrect. I just can't understand why there is so much trouble in the pilot community understanding that Newton and Bernoulli do NOT conflict in any way whatsoever, and that each explanation is correct in itself. Newton AND Bernoulli are BOTH present simultaneously on th wing at any moment lift is being created. EACH creates the other and EACH is a complete explanation for how lift is created. You can use either Newton or Bernoulli to explain lift, but the correct way to explain it is to explain how both are correct. In other words, anytime you have lift being created you have a Newton explanation AND a Bernoulli explanation occurring at the SAME TIME! -- Dudley Henriques |
#268
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"Dudley Henriques" wrote
Any article that "discounts Bernoulli" as having anything to do with lift is incorrect. I would have thought so too but I tend to put a fair amount of weight on what Garrison says when it comes to this sort of thing. You can use either Newton or Bernoulli to explain lift, but the correct way to explain it is to explain how both are correct. In other words, anytime you have lift being created you have a Newton explanation AND a Bernoulli explanation occurring at the SAME TIME! According to the article where Bernoulli falls apart is in the assumption that the air flowing over the top of the wing arrives at the trailing edge at the same time that the air flowing under the wing does, and since it has further to travel it must be going faster thereby lowering the pressure above the wing. The article states that in fact, this is exactly what does not happen - the air flowing over the wing actually arrives at the trailing edge after the air flowing under the wing. BDS |
#269
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BDS wrote:
"Dudley Henriques" wrote Any article that "discounts Bernoulli" as having anything to do with lift is incorrect. I would have thought so too but I tend to put a fair amount of weight on what Garrison says when it comes to this sort of thing. You can use either Newton or Bernoulli to explain lift, but the correct way to explain it is to explain how both are correct. In other words, anytime you have lift being created you have a Newton explanation AND a Bernoulli explanation occurring at the SAME TIME! According to the article where Bernoulli falls apart is in the assumption that the air flowing over the top of the wing arrives at the trailing edge at the same time that the air flowing under the wing does, and since it has further to travel it must be going faster thereby lowering the pressure above the wing. The article states that in fact, this is exactly what does not happen - the air flowing over the wing actually arrives at the trailing edge after the air flowing under the wing. BDS I think I see where this article has gone wrong. What Garrison is talking about is the equal transit theory, which is indeed incorrect, but it's CRITICAL that a pilot reading this completely understand that it isn't Bernoulli that is incorrect, but rather the equal transit theory that is incorrect. The equal transit theory is simply a totally incorrect INTERPRETATION of Bernoulli that has been passed around for eons by CFI's, pilots, and indeed textbooks as well. It's quite common for someone writing an article on lift to try and make a distinction that Bernoulli is incorrect by referencing the incorrect interpretations that have been out here in the community for many years. Just remember; the incorrect interpretations that misrepresent Bernoulli are in fact misrepresentations of Bernoulli, NOT proof in any way whatsoever that Bernoulli's CORRECT theory is wrong. -- Dudley Henriques |
#270
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Dudley Henriques wrote:
Any article that "discounts Bernoulli" as having anything to do with lift is incorrect. I just can't understand why there is so much trouble in the pilot community understanding that Newton and Bernoulli do NOT conflict in any way whatsoever, and that each explanation is correct in itself. Newton AND Bernoulli are BOTH present simultaneously on th wing at any moment lift is being created. EACH creates the other and EACH is a complete explanation for how lift is created. You can use either Newton or Bernoulli to explain lift, but the correct way to explain it is to explain how both are correct. In other words, anytime you have lift being created you have a Newton explanation AND a Bernoulli explanation occurring at the SAME TIME! Most people seem to want simple, one size fits all answers to everything and forget that most real life things, e.g. what causes lift and what causes cancer, are complex and can't be boiled down into a 10 second sound bite. -- Jim Pennino Remove .spam.sux to reply. |
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