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#11
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the upward sloping line on these graphs is the computed weight x arm =
moment and then the CG is read.. "Robert Moore" wrote in message ... "John T" wrote For instance, every W&B graph I've seen (Skyhawks, Skylanes, C150s, Warriors, Katanas, Tomahawks - all under 35 years old) have shown this graph using only weight/moment. All the sample loading problems I've seen have all used moment instead of arm, too. In those airplanes, the "arm" is generally fixed by the location of the seats and bagage compartment. On the graphs, the upward sloping lines each represent a different arm. Regardless of how it is presented, a w/b calculation always involves weights and arms. Moment is simply weight times the arm. Bob Moore |
#12
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"BTIZ" wrote
the upward sloping line on these graphs is the computed weight x arm = moment and then the CG is read.. In my C-172 manual, the upward sloping lines have no units. One enters the chart on the left with weight, goes over to the appropriate diagonal line (front seat, rear seat, baggage) and then drops down to the base line and reads moment. Bob Moore |
#13
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Ron Natalie wrote:
I'm sure you're confused. The CG point is always an arm. A moment tells you NOTHING about the CG. A moment of 1000 could be 1000 pounds at the datum or 1 pound 1000 units away from the datum. If you've computed the moment, you divide that by the weight to get the arm. The 1986 Cessna Skyhawk manual presents the W&B data in both Weight vs Moment and Weight vs CG. John Roncallo |
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