Is this true? Are there any physics geeks here? In my mind I am thinking about how commercial aviation CHASES weight reduction with full blown passion. It's true that the speed of commercial aircraft doesn't change a whole lot, but that's because the manufacturers match thrust to weight. So, the reason commercial aviation chases less weight is to reduce the amount of thrust needed in order to increase fuel efficiency. I think . . . . .
If Corax's statement is true, however, typically adding cannons to fighters did increase drag, so you would want to account for that. Also, anything that is an external pod (bomb locks, drop tanks, etc) would give quite a bit of drag and so should decrease speed, but I don't believe there is a "drag" variable in the calculations? Which would mean, the only way to reflect this would be to give a malice to speed based on weight. Just thinking out loud . . . .
Thanks!
Weirdly enough there's a great writeup on the effects of weight on aircraft performance on linkedin, but there's also the FAA's guidelines that give an idea. Basically more weight reduces climb speed, optimal cruise speed, manoeuvrability, rate of climb, max altitude, basically any flight characteristic of an airplane but max speed. Since airlines don't want to go faster due to drag increasing much faster as you approach the speed of sound they try to reduce weight because it allows them to go further since they get more lift for a given wings size which means smaller wings which means smaller engines which means less cost to operate, among other things gained from less weight such as climb rate and runway length requirements. Additionally It can be the case that in order to make the lift of the aircraft high enough for the weight you increase the drag (large straight wings or higher AOA etc...)and so indirectly is reduces speed.
If I'm misunderstanding anything I'd been happy to get an explanation of it.
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