Accession Number : AD0698110

Title :   CALCULATING THE SUPERSONIC SECTION OF A LAVAL NOZZLE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Dorfman,A. Sh.

Report Date : 18 AUG 1969

Pagination or Media Count : 16

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)

Descriptors :   (*LAVAL NOZZLES, SUPERSONIC CHARACTERISTICS), SURFACE ROUGHNESS, WALLS, NUMERICAL ANALYSIS, SUPERSONIC NOZZLES, USSR

Subject Categories : Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE