DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
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
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
Distribution Statement:
APPROVED FOR PUBLIC RELEASE