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#16
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Doug overstates the case a bit. Even without elevator
control it is possible to damp out the phugoid mode. I tried this on a BFR recently and I encourage the rest of you to give it a try as well. Since the phugoid is a function of airspeed/pitching moment coupling, you can damp it out by applying speedbrakes at the bottom of the cycle. This take a bit of thinking ahead, but it can be managed with practice. The United 232 crew was able to control pitch through pitch/thrust coupling. They applied collective thrust to adjust pitch and differential thrust for directional control. It was crude put effective enough to get to the runway threshold. Unfortunately, the dug s wing in on landing. It was not directly a result of the phugoid mode, though I suspect all the different modes conspired a bit. At 00:48 01 November 2003, Doug Haluza wrote: (nowhere) wrote in message news:... Yes, according to Peter Garrison's 'Aftermath' column in the November issue of 'Flying' you don't need to connect your elevator control! I quote: 'the NTSB report does not comment on the fact that a disconnected elevator does not make an ASW-20, or for that matter any other airplane, unflyable. The situation is aerodynamically no different from what occurs when the pilot removes his hand from the stick.' I think I'll start leaving the elevators off my ASW-15 now. Imagine how the reduction in drag will improve the performance! Not having to worry about pitch control will certainly cut down on the cockpit workload as well. The benefits are endless! Well, it may be flyable, but not landable! The stick free phugoid can get pretty dramatic, even with the mass and friction of the stick attached to provide some damping . If you have not tried this, you should. Keep hands completely off and keep the wings level with rudder. Let the phugoid fully develop--it's a real roller coaster ride. Close to the ground, it's a crap shoot whether you would land or crash. There was an accident a few years back in a DG-800 that had a loose nut on the elevator control. The pilot hit on the down part of the phugoid and crashed wings level. He lived, but never flew again. The same thing happened to United Flight 232, the DC-10-10, that crashed while attempting an emergency landing at the Sioux City Gateway Airport, Iowa, in 1989. After losing all hydraulics, they had no movable flight controls. They were able to fly the aircraft with differential thrust on the two wing engines, but they could not control pitch on final approach. I have not seen the article, but I'm surprised that a knowledgable person would suggest that elevator control is optional. |
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