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#19
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![]() pTooner wrote: Firstly, I am new here although I've been reading for a few days. For anyone with more knowledge than I, I keep considering building a small 4 wing aircraft. Not stacked, but two up front and two in the rear. I have read frequently of problems supposedly resulting from interference of the airflow between wings, but I can't seem to find anything very specific. I'm fairly confident that interference between the front wings (or rear) can be minimized by reasonable spacing and differing dihedral. I'm not sure what the effect of the airflow coming off the front wings will have on the rear set. I don't know whether I could remove most of the problem by having one set considerably higher (how much?) than the other set or if it is reasonable to have them on more or less the same height. The reason for the concept is trying to get a wingspan small enough to fit into a normal garage and conceivably take off and land from streets and highways. I visualise something in a two place plane that would fall into something of the appeal category of a motorcycle or small sports car. Any thoughts would be appreciated. Gerry John Roncz called a 3 surface airplane he participated in the design of "the aerodynamicists full employment act"! You will, with optimization of all the variables. be lucky to get 40% of the lift/drag ratio of an equivalent conventional planform. But the bigger problem will be control. Pitch stability, in and out of ground effect, will be a formidable problem, as will stall characteristics. Compromises needed to make the handling acceptable may make the efficiency even worse. I agree with Ernst - a low aspect ratio delta/lifting body makes more sense. Perhaps a 2 seat Facetmobile with the outer portions folding inward like a Dyke Delta. But have you looked at all the wires around most roads? Not an area I would want to use for landing and takeoff. |
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