Accession Number:

AD0625787

Title:

SIMILTUDE LAWS FOR A FLOW OF GAS IN A THIN HYPERSONIC NOZZLE,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Zhilin,Yu. L.

Report Date:

1965-10-26

Pagination or Media Count:

11.0

Abstract:

A similitude law for flow of gas in a hypersonic nozzle taking into account the interactions of the boundary layer with a potential nucleus similar to a previously established similitude law for external flow past thin bodies is obtained. Author

Descriptors:

• *NOZZLE GAS FLOW
• HYPERSONIC FLOW
• PERTURBATIONS
• SIMULATION
• USSR
• BOUNDARY LAYER

Subject Categories:

• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE