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Old Feb 28, 2004, 05:03 PM
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Dallas,TX, USA
Joined Mar 1999
834 Posts
natoquick,
I recommend that your team develpe Thrust required (drag) and thrust available data for you aircraft and engine/prop combination using payload combinitions from 0 to 25 lbs. I wrote a paper in 1991 called "Model Airplane Performance Analysis" and published it in the NFFS sympo of that year. You may want to get a copy for some of the equations and methods. I will be sending you 4 files from that paper illustrating my basis of computation.
Dick Huang
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Last edited by Dick Huang; Feb 28, 2004 at 05:09 PM.
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