Originally posted by F4UDOA:
Niklas,
Here it is power loading listed at 6.8 so the HP must be at around 1700HP
military power
Vmax=395MPH at 23000FT.
Vmax at sea level=341MPH
F4UDOA
Ok guys, I see folk quoting drag coefficients, engine power and equivalent flat plate areas and making predictions about top speeds, but we can put this on a scientific basis, we can use those values to calculate the top speed.
I've done the math and the equation can be used to calculate the top speed given the data you guys have been quoting.
I've just tested it on the F6F-5 for example and given a peak prop efficiency of 83% from an engine delivering 2000HP and wings with an area of 334ft^2 and a Cd0 of 0.0223 the top speed at sea level clocks out at 320mph. I have a published value of 318, so the calculation has less than a 1% error.
Now don't lynch me because of my data
If anyone would like to post some data sets, I'll do the calculations and post the top speeds?
Data required is:
Prop Efficiency (e)
Altitude (h)
Engine Horsepower (hp)
Wing Area (s)
Zero Lift Drag Coefficient (Cd0)
The aircraft weight and induced drag are neglected, which result in a very small error, often less than 1%.
Badboy