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On Apr 16, 9:41 am, Jose wrote:
I seem to recall recent magazine (web?) articles where the idea that you can hit your own wake while actually holding altitude, should be downplayed nowadays. You _have_ to descend a little bit to do so, How tall is the wake? Good point. Still, using the calculator at: http://www.csgnetwork.com/aircraftturninfocalc.html It's going to take about 30 seconds to fly a 360 steep turn at 100kts. My wake _should_ descend about 150' during that time (300 fpm). I can't imagine a C172 wake being tall enough to stay in my way unless something else is ocurring (me descending, or the wake staying up). Would love to hear a decent explanation. Kev |
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My wake _should_ descend about 150' during that time (300
fpm). I can't imagine a C172 wake being tall enough to stay in my way... I can. 150 feet is not tall at all for a wake. Remember, the air around the wake is also being dragged by the wake vortex. You're going to bump into something. Jose -- Get high on gasoline: fly an airplane. for Email, make the obvious change in the address. |
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Jose writes:
I can. 150 feet is not tall at all for a wake. It's extremely tall for a small aircraft. The wake would probably be about 50 feet high. Remember, the air around the wake is also being dragged by the wake vortex. But at very slow speed. Even the downwash itself is moving slowly, only a few knots. Any of the winds that one often encounters at altitude would be enough to rapidly disperse it. -- Transpose mxsmanic and gmail to reach me by e-mail. |
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In rec.aviation.piloting Mxsmanic wrote:
Jose writes: I can. 150 feet is not tall at all for a wake. It's extremely tall for a small aircraft. The wake would probably be about 50 feet high. Remember, the air around the wake is also being dragged by the wake vortex. But at very slow speed. Even the downwash itself is moving slowly, only a few knots. Any of the winds that one often encounters at altitude would be enough to rapidly disperse it. You have no idea of the altitudes or winds aloft at which most people practice maneuvers in real airplanes. Wind by itself will not "disperse" anything, it will just move it. It takes turbulant air to disperse things in the air. -- Jim Pennino Remove .spam.sux to reply. |
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In rec.aviation.piloting Mxsmanic wrote:
writes: You have no idea of the altitudes or winds aloft at which most people practice maneuvers in real airplanes. Neither does anyone else. You don't know until you get there. Another essentially true, but worthless statement that serves no purpose other than to play semantic word games. Most practice maneuvers are done in a small altitude box for reasons that Microsoft flying games do not simulate. Wind by itself will not "disperse" anything, it will just move it. Winds interacting with each other will disperse lots of things. There is no such thing as "winds" at a particular point in the sky, there is only the wind. It takes turbulant air to disperse things in the air. See above. Turbulant air is caused by differences in wind over an area. -- Jim Pennino Remove .spam.sux to reply. |
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On Apr 16, 10:22 am, Jose wrote:
My wake _should_ descend about 150' during that time (300 fpm). I can't imagine a C172 wake being tall enough to stay in my way... I can. 150 feet is not tall at all for a wake. Remember, the air around the wake is also being dragged by the wake vortex. Hmm. We're going to have to define a wake, methinks. I can't find anything about body wakes, for example. Do they give much of a bump? Glider pilots, are you listening? On the other hand, wingtip vortices are a well-researched topic, and if a Boeing 727's is only 9' in radius, it would be hard to imagine a vortex being more than 5 feet in radius for a C172, if that much. Even if larger, and sinking very slowly, it should still be 50-150' below the aircraft if the other parameters (altitude, wind) are static. Regards, Kev |
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On the other hand, wingtip vortices are a well-researched topic, and
if a Boeing 727's is only 9' in radius, cite? I remember seeing pictures of wingtip vortices (of fair sized aircraft) and they looked like they were more than 18 feet across. Jose -- Get high on gasoline: fly an airplane. for Email, make the obvious change in the address. |
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On Apr 17, 12:02 am, Jose wrote:
On the other hand, wingtip vortices are a well-researched topic, and if a Boeing 727's is only 9' in radius, cite? I remember seeing pictures of wingtip vortices (of fair sized aircraft) and they looked like they were more than 18 feet across. Sorry was not cited here, but in other posts. To repeat: http://www.airpower.maxwell.af.mil/a...ug/carten.html Yes, I would've thought much bigger too, but then they wouldn't be as much a threat so far behind an aircraft if they expanded quickly in diameter. Apparently if flaps or spoilers aren't used, the danger area behind a 747, for example, extends many more miles than we're usually taught: http://www.nasa.gov/centers/dryden/a...4-14-DFRC.html Still haven't found much on really light aircraft ( 26,000 lbs), but the concept should be the same, albeit at a much smaller amplitude. There are equations for calculating the vortex, but they seem hard to get at on the web. Of interest: wingtip vortices were first formally written about in 1907 (!), and the use of vertical fins to cut down the drag on wings, dates over a decade before that. Regards, Kev |
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Just spoke to a friend with 26,000 hours. He confirmed that DC-8 and 707
heavies certainly do get a bump as they fly through their own wake during a 360 degree constant altitude turn. He also said that some Category D simulators include the effect in their motion repertoire. Rip Kev wrote: On Apr 16, 10:22 am, Jose wrote: My wake _should_ descend about 150' during that time (300 fpm). I can't imagine a C172 wake being tall enough to stay in my way... I can. 150 feet is not tall at all for a wake. Remember, the air around the wake is also being dragged by the wake vortex. Hmm. We're going to have to define a wake, methinks. I can't find anything about body wakes, for example. Do they give much of a bump? Glider pilots, are you listening? On the other hand, wingtip vortices are a well-researched topic, and if a Boeing 727's is only 9' in radius, it would be hard to imagine a vortex being more than 5 feet in radius for a C172, if that much. Even if larger, and sinking very slowly, it should still be 50-150' below the aircraft if the other parameters (altitude, wind) are static. Regards, Kev |
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