ESDU 70008:1970
$62.40
Inviscid supersonic flow past cones at zero incidence: (i) shock angle
| Published By | Publication Date | Number of Pages |
| ESDU | 1970-07-01 | 10 |
ESDU 70008, which is one of a series of four, presents data for the shock angle of a sharp-nosed right-circular cone at zero incidence in a uniform, inviscid, supersonic airflow. The data, given in carpet form, are for upstream Mach numbers increasing from the shock detachment value to a value of 4 for cones with semi-vertex angles from zero to 50 degrees and were obtained from an exact solution of the conical flow equations.
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