Browse Standards AS681J
Historical Revised 2008-06-12

Gas Turbine Engine Performance Presentation for Computer Programs AS681J

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.
AS681K
2016-06-06
Latest
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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