silverdollar1 said:
What does physics say would be the greater vertical boost.
If the model is just circled around a horizontal plane at minimal sink speed, then altitude is gained at the quickest rate as long as the model in in the updraft. A model can continue to climb as long as it is in an updraft, but a model can only go some finite distance above the updraft shear boundary in the two mass case.
The main difference in the two air mass case for a slope site is that the model is descending in a horizontal wind during a dive, so less vertical component of aerodynamic force opposing the descent, allowing a bit more vertical speed when it reaches the shear boundary. Assume a model is flown horizontally in the updraft just below the shear boundary, it reaches some maximum speed, and is then flown upwards above the updraft, reaching some maximum altitude. The question is if the model is now flown downwards back into the updraft and then pulled upwards again, will it achieve an even higher alititude, and I'm not sure if it will. I would assume that the size of the shear boundary, speed of the updraft, and the efficiency of the model would be factors. If the slope and the induced upwash are not wide enough for the model to achieve it's maximum speed in a horiztonal glide, then the pump maneuver should allow more maximum altitude.
Trying to apply math to this problem, note that the lift is related to speed
2 while the duration of time spent doing a partial loop upwards in the updraft is related to some constant / speed. This means the impulse (force x time) should increase with increased velocity from the dive, resulting in more momentum change, the updraft decelerated more and the glider accelerated more.
In the case of extreme dynamic soaring like 468 mph, I think the models are achieving speeds greater than their terminal velocity would be in a straight dive.
silverdollar1 said:
And if you are doing aerobatics in just an updraft ... term?
I'm not aware of a special term for this, so I assume it's just aerobatics done in updraft.