Accession Number:

ADA954725

Title:

Analysis of Ejectors Used as Supersonic Propelling Nozzles for Jet Engines,

Descriptive Note:

Corporate Author:

ROYAL INST OF TECH STOCKHOLM (SWEDEN)

Personal Author(s):

Report Date:

1968-01-01

Pagination or Media Count:

197.0

Abstract:

The need of efficient exhaust systems for supersonic aircraft has caused an increasing use of ejectors as propelling nozzles. The purpose of this work is to provide analytical methods for determination of ejector characteristics and pressure distribution along the ejector wall, required for thrust performance predictions.

Subject Categories:

  • Fluid Mechanics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE