Standard

SAE AS681J

Jun 2008 Withdrawn

Existing or new amendments and versions must be purchased separately.

Language English

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Abstract

This SAE Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady-state and transient performance calculated using computer programs. It also provides for the presentation of parametric gas turbine data including performance, weight and dimensions computed by computer programs. This standard is intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier. This standard is applicable to, but not limited to the following program types: data reduction, steady-state, transient, preliminary design, study, specification, status & parametric programs.

Products specifications

Standard from SAE International
Published: June 12 2008
Withdrawn: June 6 2016
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Replaced by: SAE AS681K
Refers: SAE ARP210
Refers: SAE ARP5571
Refers: SAE ARP4868
Replaces: SAE AS681H
Refers: SAE ARP755
Refers: SAE ARP4191
Refers: SAE ARP1420

Extended editions Extended editions (0)

Version history Related Corrigenda and Amendments (0)

Version history History (2)

SAE AS681J

SAE AS681H

Abstract

Products specifications

Product Relations