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![]() "John T" wrote in message ws.com... 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. Which graph are you talking about? The CG envelope itself is almost always the CG position (arm) versus weight. The other graphs (where you follow the weight out various lines for the different positions) are just computing the moment (multiplying the arm for you). The cessna books give you the arms you can use in lieu of these charts if you really want. Recent readings revealed folks referencing balance by arm instead of moment - something I'm not used to doing or reading. 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. It raised the question in my mind whether there are charts that use weight/arm instead of weight/moment. They all do. Googling for cg graph yeilds this page, which is quite representative of just about every plane I've ever come accross... http://www.eaa838.org/wtbal.htm |
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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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