NUMERICAL SOLUTION OF SOME PROBLEMS OF GAS FLOW,
Abstract
A description is given of the numerical calculation of the potential flow in the subsonic and transonic part of a Laval nozzle, the method of computing the unsteady one-dimensional flow during explosions in the gas, the solution of the problem concerning the flow of a supersonic stream of conducting gas around blunt magnetized bodies and, finally, a calculation scheme of the numerical method of characteristics by layers, suitable for being applied to the case of calculating the flow around bodies under an angle of attack. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 16, 1966
- Accession Number
- AD0643895
Entities
People
- P. I. Chushkin
Organizations
- National Air and Space Intelligence Center