Engine N2 Turbine RPM
Hello Hubbabubba , Hello Ivan,
The new He162 panel is certainly a beautiful one, with impressive new custom instrumentation, I must say!
There is only one issue which is giving me some difficulty, and that is the RPM gauge readout. Ivan, I´m glad to hear that you seem to be getting some clarity in the jet .air file obscurities, because perhaps with your new knowledge of gauge programming, you could possibly help out here... I hope we aren´t putting too much pressure on!
For a turbojet, N2 Turbine RPM is the parameter in question, and the default gauges all give a percentage readouts that can go up to about 110% N2, depending on how it is set in the corresponding parameter in the jet engine section of the .air file. Thus, it is not a real RPM count, but reads % N2.
I had adapted the bitmap for the dial of the Bell N2 Turbine rotor gauge, and set the ,air file parameters for an idle RPM of 2800 and a maximum RPM of about 11000, in order to get reading of the standard continuous thrust specified at 1764 flb at 9500 RPM at sea-level. At the moment, this occurs at 86% throttle position, and is the basis I am going by.
It seems to be the most reliable piece of information. Of course, the 86% throttle setting will vary with changes to the .air file parameters that set idle RPM and maximum RPM.
There was a red mark on the gauge dial at 9500 RPM. It also seems that there was a general recommendation to keep to 9200 RPM for extended periods of max. continuous thrust just in case...
Maximum 30-second 2028 flb thrust is insufficient for the model to attain performance consistent with specifications at any altitude, and at least 2182 flb seem to be needed, to get a reasonable Boost-envelope. RPM is generally quoted here at 11500 RPM, but will of course vary with altitude. Inexact readouts here will not really matter, as Boost was only allowed for 30 seconds, and could only be used few occasions during a flight.
The main thing is, that with Hubbabubba´s newly made authentic dial, the needle is at the wrong angle.
Possibly a bit of gauge programming could fix it so that it fits the basic specified normal max. 1760 flb thrust at 9500 RPM, which is what I suppose a pilot would go by.
Here´s a screenshot that includes the Beckwith Gauge Set, showing the thrust values, my own adapted RPM gauge showing the 9500 RPM, and the N1 - N2% Standard jet gauge as reference, in comparison to the new gauge.
Hubbabubba: Sorry about messing up your beautiful new panel in the screenshot with all the extra ugly stuff!!
I wonder if you would have any thoughts on this?
Cheers,
Aleatorylamp