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The sides of the duct angle away, diverge from the intake opening, at an
angle of 7 degrees. A round duct would assume a section conical shape with the walls tilted 7 degrees from the centerline. The problem is that the usual distance needed for the duct to expand from the intake opening to the size of the radiator takes more length than is available in the typical prop to firewall distance. With a square or rectangular cross section duct the sides would diverge at 7 degrees relative to the centerline. What works is left and right sides diverging, or top and bottom diverging or both top, bottom and sides diverging. Most installations expand the duct more rapidly because one is moving from an in intake opening of about 55 sq. inches to a radiator of 400 to 500 sq. inches in a distance of only 18 to 24 inches (this if aprox for a 200 hp installation). There is more to this. The opening of the intake, if nearly flush to the nose bowl surface, should have rounded edges to split the air stream as an airfoil would with smooth flow both down the throat and along the cowling. An intake that sticks forward of the surface of the nose bowl can also have a rounded leading edge, but relatively sharp sheet metal edges seem to work well also...spliting the air stream before the interference of the surface of the nose bowl. There have been articles over the years, I believe, in both Sport Aviation and Kitplanes on air duct divergence and leading edge shape. but I cannot point you to a specific article. Ernest Christley wrote: Bruce A. Frank wrote: from the intake opening to the radiator. In a perfect world proper divergence of the walls of the duct should be about 7 degrees. In practical application up to 15 degrees works well. The air expands and Very informative post, Bruce. Thank you. But could you explain this? I've heard this 7 degree figure knocked around a couple of times, but have no idea what it refers to. Does it mean that if I have a square opening in the XY plane and a line extending through the middle of it in the Z plane, then an 'extrusion' of the square will form a box that moves away from the line at a rate of 7 degrees? Then the biggest question is, how does this correspond to the rounded intake plenums that I keep seeing? -- Bruce A. Frank, Editor "Ford 3.8/4.2L Engine and V-6 STOL Homebuilt Aircraft Newsletter" | Publishing interesting material| | on all aspects of alternative | | engines and homebuilt aircraft.| *------------------------------**----* \(-o-)/ AIRCRAFT PROJECTS CO. \___/ Manufacturing parts & pieces / \ for homebuilt aircraft, 0 0 TIG welding While trying to find the time to finish mine. |
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