20CC: fuel flow, thrust?
Hi guys,
What should be the expected fuel flow from a 20CC gasser engine (say, a G20Ei with a 15X6 prop) in mild cruise, non-aerobatic flight? IOW, how long should I expect a 16oz tank to last?
Also... can anyone share thrust data from the above prop at full power in an engine such as the G20Ei?
Thanks,
Bruno