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On Apr 24, 6:41 pm, tman inv@lid wrote:
Here's why I wonder about that. Let's suppose 65 KAS before and after a 180 turn from a 10 KT headwind. OK, before the turn, your groundspeed is 55KTS and after the turn your groundspeed is 75KTS. Your intertial frame of reference is tied to the g/speed, not the a/speed. So -- the kinetic energy of the aircraft and contents is about 33% higher (75/55)^2. That energy is only going to come from one place with no power -- trading in altitude (potential energy) for kinetic energy. In your world, it's gonna be pretty hard for a sailplane to circle in a drifting thermal. In my world, it's not a problem. |
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