Accession Number:

AD0754601

Title:

Special Properties of Supersonic Gas Flows in Perforated Boundaries,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1973-01-05

Pagination or Media Count:

10.0

Abstract:

The development history, operating principles, and potentialities of supersonic nozzles with perforated edges are briefly discussed. It is pointed out that the properties of supersonic flows in perforated boundaries can be used in many regions of technology. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE