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Hello everybody,
I'm trying to set the table 1507 according the paper "FS Thrust vs Altitude calculation" but I need help because I don't understand the correct workflow to do.
The paper says:
"Having established values for gross thrust (with 1507 all zeros) the next step was to put values in for 1507 using stock data.
AirWrench then gave net thrust and by subtracting that from the established gross thrust the results were compared with EngineSim values for ram drag."
I used a table 1507 with all zeros and changhing the throttle by means AW I have back the gross thrust values obtained previously with Engine Sim (this because with table 1507 all zeros, the gross thrust is equal to net thrust).
Then, the paper says:
"After only three iterations I got ram drag agreement with EngineSim within 0.03% from sea level to 36100 ft."
...and here starts the problem. What do the paper intends with "three iterations"? Do I have to use AW and EngineSim in conjunction?
Could someone kindly help me?
Thanks!!
I'm trying to set the table 1507 according the paper "FS Thrust vs Altitude calculation" but I need help because I don't understand the correct workflow to do.
The paper says:
"Having established values for gross thrust (with 1507 all zeros) the next step was to put values in for 1507 using stock data.
AirWrench then gave net thrust and by subtracting that from the established gross thrust the results were compared with EngineSim values for ram drag."
I used a table 1507 with all zeros and changhing the throttle by means AW I have back the gross thrust values obtained previously with Engine Sim (this because with table 1507 all zeros, the gross thrust is equal to net thrust).
Then, the paper says:
"After only three iterations I got ram drag agreement with EngineSim within 0.03% from sea level to 36100 ft."
...and here starts the problem. What do the paper intends with "three iterations"? Do I have to use AW and EngineSim in conjunction?
Could someone kindly help me?
Thanks!!