# My Awcgs Blogs

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## Entries in this blog

Here is a triangle, such as △ABC,∠ B as supporting an object's former vertices, Its weight is:Gn,objects behind the fulcrum weight is: Gm,Is the total weight: Ge,As shown in figure. The graph of the symbol definition is:d=AC,AB=c,AC=b,BC=a,AL=x,OL=y, tanθ=BC/AC=a/b,Cosθ=AC/AB=b/a. The problems need to be solved as follows:   1.When the object's centerline is horizontal reference line (green line) above,also is h1＞h2,θis positive angle(that is ＋3°、＋5°、＋7°、＋10°,etc),at this time B Angle (B po

## I want to win friends help---Ask about Center of Gravity solutions.

Please help me to solve this problem, it needs to calculate aircraft's centre of gravity, as follows: 1.Weight and the ARM: (1) Front wheel weight: 600kg,to Datum distance:372mm, (2) Main wheel(Wl+Wr) weight:1400kg,to Datum distance:2200mm,Wing frontier to the Datum distance:1963mm, (3) Total weight: 2000kg,   2.I need to calculate the following results: (1) The aircraft was in a horizontal status of longitudinal CG position, vertical CG position. (2) The front end of the aircr

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