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FWind

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Everything posted by FWind

  1. FWind
    losing~2780lbs just missiles, ~3000lbs with adapter. The 27 maybe is ITR, but STR 18 to 20 deg/s with half fuel without problem at 5000ft～Clean configuration.
  2. FWind
    You better read the 01-F14AAP-1.1.
  3. FWind

    AIM-54 guidance

    FWind replied to D4n's topic in DCS: F-14A & B

  4. FWind
    command inertial of AIM-54C
  5. FWind
    Thanks, ironmike:thumbup:
  6. FWind
    Some report indicate that maximum AOA for the F-14 is 74 to 77 degree. but it can't touch the AOA in DCS.
  7. FWind
    https://www.youtube.com/watch?v=Ci_Y_PLUnuI
  8. FWind
    AIM-54C include the command inertial system, but don't active command is from command message or inertial.
  9. FWind
    the AOA of 50 deg is instantaneous, the AOA of 45 deg is stable. The MAX AOA is 75-80 deg in Flight test experience with high-alpha control system techniques on the F-14 airplane.
  10. FWind
    The max AOA is around 50 deg in DCS.
  11. FWind
    Used google book search the key world of AIM-54C command inertial, you will found some Interesting Things.:)
  12. FWind
    What you found?:thumbup:
  13. FWind
    The primary contributor to this roll reversal is the negative directional stability at high angles of attack (above 18 units at 0.9 IMN, and above 21 units at 0.15 IMN).
  14. FWind
    C include command inertial guidance system. What different C and A on active command？
  15. FWind
    search the WING ROCK MODEL FOR THE F-14A AIRCRAFT
  16. FWind
    Degree is used in Stall Characteristics of the NATOPS. In Variable sweep wing design： Flight test experience with high-alpha control system techniques on the F-14 airplane：
  17. FWind
    Thanks
  18. FWind
    https://forums.eagle.ru/showpost.php?p=3879316&postcount=41
  19. FWind
    What is the Top end？:thumbup:
  20. FWind
    flight into stall in 1g, and read the NATOPS about Stall Characteristics.:book:
  21. FWind
    Maybe problem of lift.:)
  22. FWind
    Send a tacview，thanks.
  23. FWind
    Not Fix the can't got PDSTT or PSTT onto hooked TID target when it gournd speed of above 1200 knots.
  24. FWind
    In Stall Characteristics is AOA will stabilize at approximately 45° to 55° in AFCS, but AOA will stabilize at approximately 35° to 45° depending upon stores loading in DFCS.
  25. FWind
    The max angle of attack of approximately 35° in level flight.
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