Accession Number : AD0770006

Title :   Friction, Heat Exchange, and Removal of Material in the Turbulent Boundary Layer oa a Compressible High-Enthalpy Gas in Conditions of Essential Nonisothermicity, Blowing, and Negative Pressure Gradient,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Zaulichnyi,E. G.

Report Date : 29 OCT 1973

Pagination or Media Count : 12

Abstract : The report develops a numerical method for determining the ablative characteristic of a rocket motor nozzle liner.

Descriptors :   (*Rocket nozzles, Ablation), Nozzle gas flow, Skin friction, Turbulent boundary layer, Heat transfer, Compressible flow, Erosive burning, Translations, USSR

Subject Categories : Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE