ESDU 70009:1970

$62.40

Inviscid supersonic flow past cones at zero incidence: (iii) flow deflection in the conical flow field

Published By	Publication Date	Number of Pages
ESDU	1970-05-01	12

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ESDU 70009, which is one of a series of four, presents data for the deflection of a streamline in the conical flow field between the shock and the surface of a sharp-nosed right-circular cone at zero incidence in a uniform, inviscid, supersonic airflow. The data are given for upstream Mach numbers increasing from the shock detachment value to a value of 4 for cones with semi-vertex angles of 5, 10, 15, 20, 25, 30, 40 and 50 degrees and were obtained from an exact solution of the conical flow equations.