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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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