## Approximation for Distribution of Flow Properties in the Angle-of-attack Plane of Conical Flows |

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angle of attack angle-of-attack plane approximate pressure ratio approximation with exact axisymmetric conical flow axisymmetric solutions circular arc circular cones Cleary compared with exact Comparison of approximate comparison of predicted comparisons with exact compression process cone angles cone surface conical coordinate cylinder DISTRIBUTION OF FLOW distributions of velocity equation A15 equations for distributions exact numerical solutions exact solutions figure 13 flow angle flow properties free-stream function given by equation Helium inviscid and isentropic Mach numbers method of characteristics Moffett Field NASA TN plane of conical predicted and exact predicted distributions present approximation radius of curvature range of cone real gas reference 11 results from reference right-circular cones semiapex cone shadowgraphs shock angle shock wave shown in figure solutions from reference stagnation line streamline hodograph Supersonic Flow surface inclination swept-cylinder flows trigonometric identities V/Voo velocity and flow velocity and pressure wedge and swept-cylinder