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MA_VMF

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Everything posted by MA_VMF

  1. SL AoA=0 M=0.8
  2. null null
  3. М=1.1 АоА=0 М=1.2 М=1.5
  4. Условия теже 2.5М АоА=5 Су=0.62 Сх=0.219 Сya=0.62*cos(5)-0.219*sin(5)=0.5985 Cxa=0.219*cos(5)+0.62*sin(5)=0.272 nullK=2.2
  5. MA_VMF

    DCS МИГ-29A

    его PFM Тоже вызывает большие вопросы, на скоростях 700+ легко душится малейшим движением РУС
  6. MA_VMF

    DCS МИГ-29A

    да
  7. nullnull null null null
  8. Body There was no reduction of the mesh on shock waves, which gives worse results
  9. Применена другая под программа и другой метод условия М=2.5 АоА=5.Отсутствует сгущение сетки на ударных волнах nullnull
  10. These are the calculation conditions M=2, AoA=5
  11. I didn't understand the question
  12. nullMach 2 AoA=5 Drag=345.34N Lift=1822.59N
  13. This is a diagram showing the relative pitch of the grating and the angle of attack. The plans will not interact with each other nullThis is the plane of symmetry
  14. 1.5M AoA=0
  15. Do you even understand what grids exist? Different t_bar, H_bar , n grid in my calculations t_bar=1, H_bar=0.5 nulldespite the fact that there is already a mutual influence of plans in your drawing, although according to the schedule. At a speed of 2.5M, this should not be the case.
  16. I don't care what you've made up for yourself here. Once again, the conditions 2.5M and 5 AoA were set in the program. The fact that something doesn't match is your problem.
  17. L- near 2kN D-near 420-430N Only half of the steering wheel was used
  18. Mach=2.5, AoA=5 null L/D-4.5
  19. t_bar=relative grid pitch, t/b H_bar= relative height of the grid H/L n-The number of plans in the grid
  20. AoA=20, L/D=2.5
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