The first thing about the energy balance to understand is that the external input of energy to the cart system only has to equal the losses in the system plus any gain in KE of the system.
The losses of the cart system (again, all in a frame of reference where the ground can be considered stationary) are the aerodynamic drag, the rolling resistance, the drivetrain losses, and the aerodynamic losses at the propeller. It is important to note here that the negative work of the prop on the cart is not a loss, since much of it is put right back into the system, just the part lost in the drivetrain and aerodynamically are losses.
And the cart will gain KE as it accelerates from 10.72 to 10.81 m/s over the course of a second.
So starting with the aerodynamic drag, that is a force of 7.39 N acting over 10.72 m/s, for a loss to the system of 10.72 * 7.39 = 79.2 J/s.
Next the rolling resistance, a force of 37.6 N acting over 10.72 m/s gives a loss of 403.1 J/s.
Now it starts to get more complicated. The torque demand at the propeller shaft equates to a power demand of 2993.5 J/s (Watts), While the negative work on the cart from that demand equals 303.2 N * 10.72 m/s = 3250.3 J/s, giving a drivetrain loss of 3250.3 - 2993.5 = 256.8 J/s.
So far, that is 79.2 + 403.1 + 256.8 = 739.1 J/s in losses.
Skipping the aerdynamic losses at the prop for the moment, since the same calculations will be used to determine the energy input, The ke gain of the cart system can be calculated from the difference in KE after and before.
KE = 0.5 * m * v
2
before = 0.5 * 295 kg * 10.72 m/s
2 = 16950.46 J
after = 0.5 * 295 kg * 10.81 m/s
2 = 17236.27 J
Difference = 285.8 J
So far, an energy requirement of 739.1 + 285.8 = 1024.9 J
Now for the really complicated part.
From http://www.mh-aerotools.de/airfoils/propuls4.htm" , which is the same site that Javaprop comes from, there is a generic formula for propeller thrust:
Where;
T = thrust [N]
D = propeller diameter [m]
v = velocity of incoming flow [m/s]
Δv = additional velocity, acceleration by propeller [m/s]
ρ = density of fluid [kg/m³]
Since I already have everything except Δv, I have to solve for that, which results in a quadratic equation that is too messy to post unless absolutely necessary. But I need that value both for the KE loss of the air and the prop's aerodynamic losses.
Long story short, I get a Δv of 2.417 m/s.
With that in hand I move to the "Engine Power" formula on that same page, to get the minimum power, assuming no losses at all, for a propeller to generate that thrust in those conditions.
Which results in a power of 2473.6 W, which is far less than the 2993.5 W that is actually at the shaft. In fact, the difference is the aerodynamic losses at the prop.
So those losses are 2993.5 - 2473.6 = 519.9 J/s
For total losses and KE gain of the cart system of 519.9 + 1024.9 = 1544.8 J/s
Now, for the KE loss of the air that is actually transferred to the cart, I need the mass of the air that is decelerated, and how fast it was going before and after.
The thrust formula above is actually F = ma, where everything on the right side except for the last Δv is the mass (it calculates the volume of the cylinder of air and multiplies by density), and the last Δv is the acceleration.
So using that part to calculate the mass results in a mass of 155.79 kg.
The KE of the air before the cart moves through it is 0.5 * 155.79 kg * 5.36
2 = 2238 J
The air is decelerated by 2.417 m/s, so its velocity after the cart moves through it is 5.36 - 2.417 = 2.94 m/s;
so its KE will now be 0.5 * 155.79 kg * 2.94
2 = 673.3 J
For an energy input to the cart system of 2238 - 673.3 = 1564.7 J/s
So we have 1564.7 J/s into the system, and 1544.8 either lost, or gained in KE, by the cart system. Close enough considering all the rounding I did, and the lack of using calculus for really precise answers.