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Tony Nijhuis' lysander!


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Tony, during the design process the weight and CofG of the aircraft is calculated by the Weights department, these are fundamental inputs to the overall design and stressing of the airframe. Part of the certification requirements is to state the max allowable weight of the a/c and also the CofG fore and aft positions. Part of the flight testing is to fly the aircraft at these limits and show it has acceptable characteristics.  You can check the calcs by supporting each wheel on a set of scales (actually  load cells) which gives you the distribution of the reaction loads to the weight of the a/c. From these measurements the total weight of the a/c, and its CofG position, can be calculated.  Modern airliners have computers which calc the CofG as a function of fuel, passengers, cargo and luggage weight - it's up to the pilot to check that weight and CofG are within limits before take-off.
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Posted by Peter Savage on 18/10/2009 20:02:40:
On aircraft they weight all the parts before constructing the prototype and move it around, you can put two prongs under the wings and lift it up!
 
It tends not to matter as much with full size aircraft.
 
 
A too far aft C of G affects full size as well as models Peter. All aircraft have a graph in their Flight Manuals that show the C of G limits and as was said earlier, it is up to the pilot to check the loading before flight.
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