Standard

SAE AIR1191

May 1989 Withdrawn

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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: 1 May 1989
Withdrawn: 1 March 1999
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

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Replaced by: SAE AIR1191A

SAE AIR1191

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