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,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Zaulichnyi,E. G.

Report Date:

1973-10-29

Pagination or Media Count:

12.0

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