CALCULATING THE SUPERSONIC SECTION OF A LAVAL NOZZLE,
Abstract
An analytical method for calculating the supersonic part of a Laval nozzle is presented. This method permits a simplification of the calculation of the supersonic part of a Laval nozzle by omitting the complicated graphical method. Nozzles with smooth walls and those with edges are considered. The analytical calculation of the supersonic part of the nozzle is done by the approximation method of S. A. Khristianovich. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 18, 1969
- Accession Number
- AD0698110
Entities
People
- A. Sh. Dorfman
Organizations
- National Air and Space Intelligence Center