Accession Number:

AD0645826

Title:

DETERMINATION OF THE PARAMETERS OF SUPERSONIC TWO-DIMENSIONAL FLOWS OF GAS,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1966-09-12

Pagination or Media Count:

17.0

Abstract:

A numerical solution to a whole series of problems of gas dynamics was obtained with the aid of a method of integral relationships. This method has advantages in that it reduces a system of equations in partial derivatives to an approximating system of ordinary differential equations. It requires a small computer memory and leads to simple programs. Finally, this method allows conducting a continuous calculation through the breaks inside the region of the flow, which is significant in the case of the appearnace of secondary shock waves during supersonic flow-around of bodies. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE