CALCULATION OF THE AXISYMMETRIC ISENTROPIC FLOW OF A REAL GAS
Abstract
The rise in the temperatures used in aerodynamics requires the development and use of new methods for calculating t e flow of a gas having arbitrary thermodynamic properties. The present work is devote to a calculation of axi ymmetrical supersonic nozzles. Experience accumulated in calculating isentropic flows of a real gas using el ctronic comput rs is presented. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 29, 1962
- Accession Number
- AD0286579
Entities
People
- A.n. Krayko
- O.n. Katskova
Organizations
- National Air and Space Intelligence Center