THE COANDA/REFRACTION CONCEPT FOR GAS TURBINE ENGINE TEST CELL NOISE SUPPRESSION

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

14-02-2013

Publisher

SAE International

FOREWORD
Changes in this revision are format/editorial only
1 SCOPE
2 REFERENCES
3 TEST CELL/SYSTEM NOISE SUPPRESSION REQUIREMENTS
    3.1 General
    3.2 Test Cell/System Design
    3.3 Acoustic Properties
4 OPERATIONAL NEED
    4.1 General
    4.2 Military Procurements
    4.3 Disadvantages
5 THE COANDA/REFRACTION CONCEPT
    5.1 General
    5.2 Concept Definition
    5.3 The Coanda Effect
    5.4 Acoustic Refraction
    5.5 Application to Noise Suppression

Specifies information on how military/commercial/gas turbine engine test cell/system users may benefit from this unique Coanda//refraction concept.

Committee	EG-1E
DocumentType	Standard
Pages	24
ProductNote	THIS STANDARD IS STABILIZED
PublisherName	SAE International
Status	Current
Supersedes	SAE AIR 1813 : 1998

ANSI S12.76 : 2017

METHODS FOR MEASUREMENT OF SUPERSONIC JET NOISE FROM UNINSTALLED MILITARY AIRCRAFT ENGINES

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SAE AIR 1813 : 2013

Current

Table of Contents

Abstract

General Product Information

Standards Referenced By This Book

Category

Subcategory

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