Accession Number:

AD0679803

Title:

INCREASING NOZZLE THRUST BY FLOW ROTATION,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

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.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE