Hawk_5 Posted December 15, 2013 Share Posted December 15, 2013 Oh dear, that old argument has raised its head again?! Leaving the room now. Hawk_5 Modules: A10C, BS2, FC3, P51, CA, UH-1H, Mi-8MTV2 System: Gigabyte GA-X79UP4 MB, intel 3930k, Coolermaster Siedon 120M liquid cooled, Corsair Vengence Red 16GB 2133Mhz, Gigabyte Geforce GTX680 2GB Super o'clk, intel 520 SSD 240GB, Seagate Barracuda 2TB HD, Coolermaster Silent Pro 800W PS, Coolermaster CM690 II Case Link to comment Share on other sites More sharing options...
Scarecrow Posted December 15, 2013 Share Posted December 15, 2013 How about total protonic reversal? ;):) That would be bad. Very bad ;) Link to comment Share on other sites More sharing options...
8core Posted December 15, 2013 Share Posted December 15, 2013 Nope, they are games. Even how hard you wanna belive that you don't play game in your home pit ;) DCS IS GAME. :smartass: :thumbup: Link to comment Share on other sites More sharing options...
8core Posted December 15, 2013 Share Posted December 15, 2013 I can't believe I just spent an hour making this, but it had to be done. :lol: Great job ! ! ! Nice really nice ! ! ! Link to comment Share on other sites More sharing options...
Silver_Dragon Posted January 2, 2014 Author Share Posted January 2, 2014 Albatros team work on a AEM(T) http://forums.eagle.ru/showpost.php?p=1960698&postcount=398 Advanced Turbofan Engine Model I began work on this new fully dynamic engine model back in October, but it has not been implemented into the simulator at this point, so many things are still subject to change. However, I thought I would pass along some details about the planned features of this new turbofan engine model for the L-39. So far, I have written the entire engine model into a standalone program that runs at the same frequency as the DCS flight model and reads my throttle inputs in real time to simulate realistic dynamic conditions. I also view the output of the engine conditions in real time in several performance graphs. Improved Thermodynamic Model that accounts for enthalpy changes across each subsection of the engine given inefficiencies and current dynamic conditions Inertial Twin Spool Rotor Modeling Aerodynamic blade drag for each compressor/turbine stage Fuel Governor with a simple control algorithm to maintain sufficient fuel pressure at varying altitudes and airspeeds Compressor/Turbine Efficiency Curves based on airflow and rotor speed Two Anti-Surge Bleed Valves affect performance of the engine in the specified ranges for the L-39 Combustion efficiency dependent on Fuel/Air ratio Air-starter Modeling of initial engine spool up Light-off produces correct RPM acceleration and combustion allows for self-sustaining idle conditions etc. An example output from a slam acceleration/deceleration test in an early version of engine and fuel controller. Link to comment Share on other sites More sharing options...
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