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Experimental Aerodynamic Characteristics of 120 Deg Included-Angle Cone with Attached and Separated 20 Deg Included-Angle Cone at Mach Numbers of 2.36 and 2.70

机译:具有附加和分离的20度包角锥的120度包角锥的实验气动特性,马赫数为2.36和2.70

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An investigation has been conducted in a unitary plan wind tunnel to determine the aerodynamic characteristics of two different size blunt 120 deg-included-angle cones behind a 20 deg-included-angle cone. Forces and moments were measured at Mach numbers of 2.36 and 2.70, longitudinal separation distances from 0 to 3.5 body diameters, lateral (side) distances from 0 to 0.50 body diameter, angles of attack of the 120 deg-included-angle cone from 0.5 deg to 22 deg, angles of attack of the 20 deg-included-angle cone from 0 deg to 180 deg, and a Reynolds number of one million per foot. Large variations in pitching-moment, normal-force, and axial-force coefficients were noted for both Mach numbers and all longitudinal distances for the 120 deg cones in the wake of a 20 deg cone. (Author)

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