Andy Ross tried again!

> Vivian Meazza wrote:
> > As does this (2):
> >             cruise-speed="308" cruise-rpm="2850"
> >
> > This does not (3):
> >             cruise-speed="308" cruise-rpm="1360"
> 
> Again, these are *wildly* different propoellers you are
> specifying.  The second one is going to end up with four (!) 
> times the force coefficient.  In general, multiplying any 
> number in the configuration file by a factor of two and 
> expecting the aircraft to perform similarly just isn't going 
> to work.  Is there another typo?  What are you trying to accomplish?
> 
> Andy
> 

The engine I'm trying to specify developed 1140 HP at engine revolutions of
2850 rpm at a boost pressure of 9 psi. It was fitted with 1:0.477 reduction
gearing, which I think means that the propeller turned at 1360 rpm. Thus, if
I have understood all of the various emails correctly, leads to a
specification file:

        eng-power="1140"                engine power output = 1140 HP 
        eng-rpm="2850"          @ 2850 rpm (supercharged)

        turbo-mul="2"           Turbo multiplication factor = 2

        wastegate-mp="48"               Boost Control Valve = 48 in Hg
absolute
        cruise-alt="17500"      Cruise altitude = 17500 ft   
        cruise-speed="308"      cruise speed at cruise altitude = 308 kts
        cruise-power="1140"     Power absorbed by propeller at cruise = 1140
HP
        cruise-rpm="1360"               Propeller cruise rpm 2850 * 0.477 =
1360 rpm
        takeoff-power="900"     take off numbers 
        takeoff-rpm="1200"
        manual-pitch="true"
        gear-ratio = "0.477"    reduction gear of 1:0.477

I'm reasonably confident that the numbers are in accordance with the
published data for the engine. This results in a YASIM output;
                
                Iterations: 1
                Drag Coefficient: 1000.000000
                Lift Ratio: 1.000000
                Cruise AoA: 0.000000
                Tail Incidence: -0.00000
                Approach Elevator: 0.000000
                CG: -2.528, 0.000, -0.270

FGFS locks up attempting to run with these settings, not unexpectedly.

I made an alternative assumption as an experiment: that cruise-rpm was the
engine rpm at cruise - 2850. They are also about the lowest values for which
YASim converges. With these settings, YASim converges with these results:
                
                Iterations: 2320
                Drag Coefficient: 6.279826
                Lift Ratio: 360.380524
                Cruise AoA: 0.770977
                Tail Incidence: -0.8144328
                Approach Elevator: 0.939014
                CG: -2.523, 0.000, -0.276

FGFS runs with this input, but when throttle = 1 engine rpm = 6928, which is
as expected for a propeller rpm of 2850 and a gear ratio of 0.477. I had
hoped to see the engine rpm stay constant, and the propeller rpm to drop,
but, as I say, I was just experimenting.  Apart from the engine rpm the
model performs well with these settings. I think we have to assume that
either the published engine parameters are outside YASim's calculations in
some way, or that I still have some fundamental misunderstanding of what
goes where in the file. 

Sorry to be a nuisance with all these queries, and thank you for your
patience and help.

Regards

Vivian

 



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