Abstract: In a blade shape creation program and method, a camber line defining equation for defining a camber line to be defined on a cross section of a blade shape is constructed by a cubic function as a first function defining a leading edge camber line on a leading edge side of a maximum camber point on the camber line, and a cubic function as a second function defining a trailing edge camber line on a trailing edge side of the maximum camber point on the camber line; is defined, with a chord length, a position of maximum camber, a maximum camber value, an inflow angle, and a discharge angle of the camber line being taken as design factors; and has the boundary condition that the first function and the second function have tangents continuous with each other at the maximum camber point.

Abstract: A truck 1 includes a cab 3 in which a driver's seat is provided, a van 5 provided rearward of the cab and serving as a load container, wheels 7a, 7b, 7c, and 7d, etc. These components are attached to frame members 9a, 9b, 9c, 9d, 9e, 9f, etc. An engine 13 is provided between the frame members 9a and 9b. A drive-force transmission apparatus which includes a clutch 15, a transmission 17, etc. is provided rearward of the engine 13 so as to transmit drive force from the engine 13 to the wheels (driven wheels 7b and 7d). A radiator 19 is provided forward of the engine 13 so as to cool the engine 13. A windbreaking plate 25 is provided above a portion of the engine 13 exposed from a gap 30 between the cab 3 and the van 5 so as to prevent a downward air flow 26 from hitting the engine 13 to thereby hinder the flow of radiator intake air 32.

Abstract: A shroud 15 attached to an air discharge side of a radiator 13 narrows toward a centrifugal-flow-type rotary fan 11 and forms a cylindrical shape. A surrounding portion 17 is provided so as to surround the rotary fan 11, and a guide portion 19 extending in the centrifugal direction of the rotary fan 11 is provided at the end of the surrounding portion 17. The length of the guide portion 19 is about 6% the diameter of the rotary fan 11. Since this mitigates turbulence of centrifugally flowing air 21 flowing out of the rotary fan 11 and suppress a drop in the amount of air passing through the radiator 13, the cooling capacity of the radiator 13 can be enhanced.

Abstract: A shroud 15 attached to an air discharge side of a radiator 13 narrows toward a centrifugal-flow-type rotary fan 11 and forms a cylindrical shape. A surrounding portion 17 is provided so as to surround the rotary fan 11. A guide portion 23 extending in the centrifugal direction of the rotary fan 11 is provided at a circumferential edge portion of the surrounding portion 17. A cylindrical portion 19, which is smaller in diameter than the surrounding portion 17 is provided inside the surrounding portion 17, and an upper portion of the cylindrical portion 19 is fixed to the wall surface of the shroud 15. A lower portion of the cylindrical portion 19 is fixed by a fixing portion 21 having an inner diameter equal to the diameter of the cylindrical portion and an outer diameter equal to the diameter of the surrounding portion 17.

Abstract: In a blade shape creation program and method, a camber line defining equation for defining a camber line to be defined on a cross section of a blade shape is constructed by a cubic function as a first function defining a leading edge camber line on a leading edge side of a maximum camber point on the camber line, and a cubic function as a second function defining a trailing edge camber line on a trailing edge side of the maximum camber point on the camber line; is defined, with a chord length, a position of maximum camber, a maximum camber value, an inflow angle, and a discharge angle of the camber line being taken as design factors; and has the boundary condition that the first function and the second function have tangents continuous with each other at the maximum camber point.

Abstract: In a blade shape creation program and method, a blade thickness function defining equation is constructed by a cubic function as a first function defining a leading edge blade thickness function on a leading edge side of a maximum blade thickness point of the blade thickness function, and a cubic function as a second function defining a trailing edge blade thickness function on a trailing edge side of the maximum blade thickness point; is defined, with a camber line length, a position of maximum blade thickness, a maximum blade thickness value, a leading edge blade thickness change rate, a trailing edge blade thickness change rate, a leading edge blade thickness value, and a trailing edge blade thickness value being taken as design factors, and has a boundary condition that the first function and the second function have tangents continuous with each other at the maximum blade thickness point.