Accession Number:

AD0679803

Title:

INCREASING NOZZLE THRUST BY FLOW ROTATION,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Naumova,I. N.
• Shmyglevskii,Yu. D.

Report Date:

1968-04-05

Pagination or Media Count:

11.0

Abstract:

An analysis was made of the thrust obtainable with a rotating gas stream. A formula was obtained for the overall thrust.

Descriptors:

• *SUPERSONIC NOZZLES
• *THRUST
• VORTICES
• NOZZLE GAS FLOW
• USSR

Subject Categories:

• Aerodynamics
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE