Standard

SAE AIR1191A

Mar 1999 Current

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Language English

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Abstract

A general method for the preliminary design of a single, straight-sided, low subsonic ejector is presented. The method is based on the information presented in References 1, 2, 3, and 4, and utilizes analytical and empirical data for the sizing of the ejector mixing duct diameter and flow length. The low subsonic restriction applies because compressibility effects were not included in the development of the basic design equations. The equations are restricted to applications where Mach numbers within the ejector primary or secondary flow paths are equal to or less than 0.3.

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Standard from SAE International
Published: March 1 1999
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

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Replaces: SAE AIR1191

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SAE AIR1191A

SAE AIR1191

Abstract

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