2793884

ESDU 70008 [ Active ]

Inviscid supersonic flow past cones at zero incidence: (i) shock angle.

standard by Engineering Sciences Data Unit , 07/01/1970

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Full Description

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.

 

Product Details

Edition:
70
Published:
07/01/1970
Number of Pages:
6
File Size:
1 file , 160 KB
Product Code(s):
3, 3