Shortround6
Major General
Intuitively that makes perfect sense, but compressibility effects were known since the 1700-1800's on some level, but rarely factored into early aircraft designs because they flew nowhere near fast enough to cause trouble (except the props).
I'm wondering if something like that applied to attempting to extract exhaust thrust from the engine system, or at the very least not really pursuing it in any degree because of the fact that
- Most early engines didn't produce all that much horsepower, so the amount of thrust to be gained by a creative exhaust pipe set-up wouldn't have been worth it
- Most early engines didn't have particularly high manifold pressures, so it would have interfered with scavenging
- Most early engines were naturally aspirated or used minimal supercharging, and were not capable of propelling an aircraft high enough to make use of it
- Most early aircraft were not capable of flying fast enough to make use of such a thing
Okay
I'm confused about something. Some things increase to the square of velocity, others are proportional.
I keep mixing things up
mass times velocity gives you momentum, Mass times velocity squared gives you energy.
we can break it down a bit by looking at a rifle. Bullet weight times velocity squared gives us the energy of the bullet (it's ability to do work, like punch through an obstacle) but when figuring recoil we take the weight of the bullet times velocity (NOT squared) plus the weight of the propellent times the escape velocity of the gas at the muzzle and then divide by the weight of the rifle to give us the velocity of the rifle moving backwards. Then we use the mass/weight of the rifle times it's recoil velocity squared to get the recoil energy.
Drag gets a bit stranger