DETERMINATION OF THE PARAMETERS OF SUPERSONIC TWO-DIMENSIONAL FLOWS OF GAS,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 12, 1966
- Accession Number
- AD0645826
Entities
People
- Li Li-kan
- P. I. Chushkin
Organizations
- National Air and Space Intelligence Center