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  • Posted By: sneakers321 @ 08/24/2009 12:38:03 AM



    maximum normal requirement 146.76. 0.323333333333333333333333333333333
    611.855670103092783505154639175258~116.917333333333333333333333332113
    @ 57 feet 1.92 inches vertical stabilizer setting basic setting actual setting 57 feet 1.43 inches
    1.69207873369218137031292765258644
    361.599999999999999999999999999966
    57.8812348831249999999999999615625 feet horizontal stabilizer

    Current indication is that the distance currently utilized of the vertical stabilizer on the existing plane is not correct, stress however on the pitot tubes is inherent however @ 4.162.

    @ 50.8015 variance 54.96 @ 37.38
    -2800
    0.610847172599873845255358860632794
    -0.347930984968499043269253709298568 ( horizontal stabilizer possibly commanding a drop) significant loss of lift
    57.8675 feet @ 6870.60474417512026948522216059601 possible neutral laminants required
    100.312026002166847237269772481006 approaching supersonic air rate however ratio may not be continued for elected for the fact that it might average too much weight anyways as above 940.46. This would cause the demand of the forward wings to lift and the weight of the air returning would be placed upon the vertical stabilizer which if exactly set and set by coordination of the other aspects of the design by their measurements @ 57 feet 1 inch would command the plane to degrade its altitude during its' flight path therefore utilization of said distance as in doubt from the formation of ice. 0.101465930917018765728542591602425 because it is actually requesting a new setting of 57 feet 1.41~(1.43 inches), avg 47 inches @ 6.35 ratio.
    current set is 57 feet 1 inch 982.108715005567823237067599787867 a maximum 7.166-5 7.1035 363 (27) WARNING possible breakage of vibratory characterization present and located, would not proceed with the current horizontal stabilizer distance as such as needing additional lift and placement of a redundant system which alternates to during stormy weather, vibratory characteristics would attract ice formation and may interfere directly with the lift of the plane, recommended testing in wind tunnel with liquid O2 directly of the horizontal tail stabilizers. However alignments of electronic ice prevention boxes should be mounted within the wingsets and the vertical stabilizer preventing ice approaching and amassing toward the wings and the horizontal stabilizers and activated for use in bad weather. It is possible that a reduction of lift if sufficient ice is present and not being disbanded if approaching the stabilizer set.
    if set at 57 feet 1.23 inches vertical stabilizer distance requested, ratio is 6.398 is additionally as requested and appears to be fully functional reasonable stability needs to be established if also wishing with an alternate set of horizontal stabilizers, liquid O2 ice testing also recommended, otherwise 57 feet 1.43 inches vertical stabilizer recommended.

  • Posted By: sneakers321 @ 08/22/2009 6:36:44 PM

    maximum normal requirement
    57.8812348831249999999999999615625 feet @ 55.19

    Current indication is that the distance currently utilized on the existing plane is not correct stress however on the pitot tubes is inherent however @ 4.162.

    @ 50.8015
    57.8675 feet possible neutral laminants required

    pardon the additional comment.

  • Posted By: sneakers321 @ 08/21/2009 10:22:25 PM

    Just one more comment, thank you. If and when .41 cu feet is averaged against the sensors in a storm situation it could lead to the actual sensors themselves sustaining damage which is not repairable. So my idea is not to use the 41, or get some pitot tubes that can withstand that type of wind, or they will probably break again.

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