Quote:
Originally Posted by Crumpp
You lose the forest for the trees as all you can see is your one specific solution you have been taught to parrot. You don't seem to understand that the force of weight continues to have the same affect on the aircraft whether it is at high velocity or low velocity.
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This is actually your problem here; you use the formula which wrongly assumes constant Cl/Cd relation for the question in hand. My solution correctly changes the Cl/Cd relation to reach new balance between the drag and thrust. Thus, the effect is not the same nor the results comparable.
This is the principal difference between these approaches and allready pointed out in the posts #21, #24... and also #150 of this thread, which you continously misquote and try use to for exactly opposite purpose, it was originally posted.
But as allready seen in this thread, there is no limit how far you will go on this. In the AH board you were banned for this kind of manners and I've been told that the same happened in the ww2aircraft.net, where I have never posted.