Standard

SAE AS681K

Jun 2016 Withdrawn

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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, and parametric programs.

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Standard from SAE International
Published: June 6 2016
Withdrawn: August 21 2023
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Replaced by: SAE AS681L
Refers: SAE ARP210
Replaces: SAE AS681J
Refers: SAE ARP5571
Refers: SAE ARP4868
Refers: SAE ARP755
Refers: SAE ARP4191
Refers: SAE ARP1420

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Version history Related Corrigenda and Amendments (0)

Version history History (2)

SAE AS681K

SAE AS681J

Abstract

Products specifications

Product Relations