Clmax figures for Soviet fighters?

Discussion in 'Engineering Retrospective' started by HoHun, Sep 17, 2006.

  1. HoHun

    HoHun FH Beta Tester

    Joined:
    Sep 22, 2001
    Messages:
    2,643
    Hi everyone,

    As I know the forum members have done some in-depth research of the Soviet fighters, I hope the information I'm looking for is already available :)

    Maybe it's already on this board, but unfortunately, I don't read Russian :-(

    Anyway: What Clmax figures do you have for the Soviet fighter?

    I'm looking for the Clmax figures for the entire line-up:

    I-153
    I-16
    LaGG-1/3
    La-5/F/FN/-7
    MiG-1/3
    Yak-1/9
    Yak-7/3

    (Preferably, I'd like to know the Clmax power-off, clean, even if that's a bit lower than Clmax power-on, because it makes it easier to compare.)

    For the La-5, I found it has a NACA 23xxx wing an probably a lift coefficient around 1.2. The Yaks seem to have Clark YH wings and (so I suspect) probably around 1.3. However, I'm not sure about the effect of the leading-edge slat on the Lavochkin aircraft, and my guess about the Yak is inaccurate at best. I don't have any data on the MiG or I-16.

    Your help would be much appreciated :)

    Regards,

    Henning (HoHun)
     
    HoHun, Sep 17, 2006
    #1
  2. -exec-

    -exec- FH Consultant

    Joined:
    Jan 29, 2000
    Messages:
    24,690
    Location:
    xUSSR
    помогите товарищу, люююди :)
    спрашивает Clmax для названных аппаратов, лучше без мотора (говорит - при тяге параметр выше).

    кстати, взамен можно попросить то же самое по другим ;)
     
    -exec-, Sep 17, 2006
    #2