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On Sat, 19 Dec 2020 16:24:01 -0800, Eric Greenwell wrote:
As we all know, tow ropes do not break in steady flight! It's dynamic loads from turbulence and piloting that put the peak loads on the rope; nonetheless, the average load (say, over 1 minute) will be close to the simple physics of lifting the weight of the glider at the rate of climb. That number doesn't have much value in our operational choices, I think. Yep. I only made an attempt at calculating it a while back because I was curious about the tension in the tow rope under during normal operating conditions. I think there are other towing factors that are probably more important to understand. For instance, the aerodynamics of towing our gliders with our typical tow planes are quite different from those of the majority of military glider tows because almost for virtually all military towing the tow plane has a bigger wingspan than the glider. This was the case for all British and US operations in WW2 and for most German towing too. In fact, the only cases I've found where the military glider was bigger span than the tug was the ME 321 Gigant (the Gigant was bigger than its He-111Z towplane) and the DFS 230 when it was being towed by a BF-109 or Bf-110. Conversely the only civilian gliders I'm aware of that are smaller than their towplane are Perlan 2 when the Grob G520 Egrett is towing it and an SGS 1-26 behind a Piper Cub. This can matter, because if the glider is smaller than its tug, its entire wing is operating in the downwash from the tug's wing, while if the glider is bigger than its tug, then, while the inner part of its wing is in the downwash behind the tug's wing, the outer parts of its wing project through the tug's tip turbulence and into the upwash created by the outer parts of the tug's tip vortex and may well give an tendency for the glider to tip stall if the tow speed is too slow. -- -- Martin | martin at Gregorie | gregorie dot org |
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