국내 최대 기계 및 로봇 연구정보

공학설계D/B

공학설계D/B 게시판 내용
Volume Title	Aerodynamics
Volume No	GENERAL - Organisation, properties of gases, isentropic flow and shock waves.
DATA Title	Inviscid supersonic flow past cones at zero incidence: (i) shock angle.
DATA Item	70008
KEYWORD	angle, cone, flow, shock, supersonic, wave
ISBN
ABSTRACT	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.