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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,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Pagination or Media Count:
The report develops a numerical method for determining the ablative characteristic of a rocket motor nozzle liner.
APPROVED FOR PUBLIC RELEASE