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HS p-75
I have a question on canard elevator surface area, D/R and Expo.
My present build is here:http://www.rcgroups.com/forums/showp...9&postcount=15 and continues through to http://www.rcgroups.com/forums/showp...1&postcount=26. Canard area is 20% of the main wing. Canard is a E217 and will have 3 degrees positive incidence. Main wing is a E197 with 1 degee incidence with outer control surface as ailerons and inner as secondary elevators. Secondary elevators are there to help in turns with about 5 degrees down and 20 degrees up max travel. Airfoil coenfecants are set up so the wings will have the proper stalls for canard aircraft. I just do not know the set up for the canard elevator and if the secondary elevator is really needed Thanks |
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Joined Jun 2005
2,306 Posts
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P901, Your design looks good to me. I do not believe that you will need elevators at the rear since you have rather long moment arm up front. Also the moment arm for the rear elevators will be short. The airfoil selections look good with the main wing stalling after the canard.
Charles |
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So I will use about 30% of the area of the canard as the elevator and about 1/2 span of the main wing section as the aileron. I guess control throws and expos will be up to experimentation. Thanks |
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And have een lurking in this thread and reading the experts opinions and have been learning allot. After this comes the Lockheed L-133 http://www.rcgroups.com/forums/showt...ghlight=lockhe Thanks and will need suggestions. |
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