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Barao

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Posts posted by Barao

  1. I tried two times, after I rejoin whit Colt (TACAN 18 out - 20 NM), DCS stop to work and crash.

     

    This occurs before and after corrent DCS update 1.577.

     

    PS: It's a great campaign

  2. Ok guys, I asked my fighter pilot friend to test the module, I attached the trk of his flight.

     

    His conclusions, according to what he can speak without compromising the secrecy. It is in agreement with the graph posted here in the forum, which is not totally wrong, but the performance is a bit degraded.

     

    According to him, the 2000 supports 9 g at 10000 ft and still accelerate a little without external store, the limit is the resistance of the pilot.

    The reason that the energy is degraded is a bit accelerated in DCS.

    Small adjustments are needed, it's almost there

    M2000 IPEV.trk

  3. I was with the AOA slightly higher than 15º (I will test again), nose down in a full AB dive, and the airplanes do not gain a positive attitude to regain speed and flight level. I know that the drag in this situation reduces the thrust, but it is exaggerated.

     

    I know that a lot of the required data is confidential, but I think a conversation between the team and some M-2000 pilot could at least reduce the mistakes without compromising the secrecy. This is because the team has competence to understand what the professional describes, it would be something more technical than this our debate.

     

    This is a client's suggestion.

  4. I do not know the exact numbers, and my English is too bad to explain details.

    But I think we all know that something is wrong. I do not know exactly what.

     

    I hope the company will find the problem before the release version.

     

    Even so, I will continue to fly M-2000, It's a great project and a fun module.

     

    I only expose my impressions based on the experience of a friend who knows the actual machine and based on my feeling that something is wrong

  5.  

    General rule of thumb:

    Stay below 15° AoA: thrust > drag = you can accelerate.

    Go beyond 15° AoA: drag > thrust.

     

     

    This is too binary. There must be a transition algorithm to simulate the increase in drag to the delta wing.

    And yes, I noticed this relationship with the 15° AOA, and I say that this transition between the drag-power relationship is exaggerated.

     

    And something else, being nose-down, diving in full AB, even if the AOA exceeds a little 15°, there must be an acceleration, until a stone accelerates in a fall.

    The algorithm that controls the drag-lift transition can not be the same for horizontal and vertical flight.

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