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
Descriptors:
Subject Categories:
- Fluid Mechanics