Very nice.
Interesting how you guys are going to model the failures, I'm actually curious about a nozzle failure in DCS.
If the nozzle gets stuck in a transition from MIL to MAX AB, where the nozzle must open in order to change the nozzle area and also keep the backpressure under the limits, that actually can overheat the engine, is there any word about this? Excessive backpressure could make the temperature between turbines (Normally T5) exceed its limits. is that going to be modeled too?
Also, last time I asked you guys about Ram Drag, and the lack of it in the last update (by Heatblur too). BlackLion gently sent me a message saying it wasn't modeled due to lack of documentation, but you guys actually found some documents about the F-14's inlet efficiency. How's that working for you guys? Not sure if that's a sensitive question but I'm curious :P
Thanks!