Browse Standards AS681K
Historical REVISED 2016-06-06

Gas Turbine Engine Performance Presentation for Computer Programs AS681K

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.
AS681L
2023-08-21
Latest
Revised
AS681K
2016-06-06
Historical
Revised
AS681J
2008-06-12
Historical
Revised
AS681H
1999-03-01
Historical
Revised
AS681G
1996-09-01
Historical
Revised
AS681F
1991-10-28
Historical
Revised
AS681E
1982-10-01
Historical
Revised
AS681D
1982-10-01
Historical
Revised
AS681C
1974-04-15
Historical
Revised

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