Accession Number : ADA954725
Title : Analysis of Ejectors Used as Supersonic Propelling Nozzles for Jet Engines,
Corporate Author : ROYAL INST OF TECH STOCKHOLM (SWEDEN)
Personal Author(s) : Ahren,B.
Report Date : 1968
Pagination or Media Count : 197
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.
Descriptors : *DETERMINATION, EJECTORS, EXHAUST SYSTEMS, JET ENGINES, NOZZLES, PRESSURE DISTRIBUTION, PROPELLING CHARGES, SUPERSONIC AIRCRAFT, SUPERSONIC NOZZLES, WALLS
Subject Categories : Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE