Browse Standards AS681G
Historical Revised 1996-09-01

Gas Turbine Engine Steady-State and Transient Performance Presentation for Digital Computer Programs AS681G

This Aerospace Standard (AS) provides a method for the presentation of gas turbine engine steady-state and/or transient performance as calculated by means of digital computer programs. It also provides a method for the presentation of gas turbine parametric performance, weight and dimensions by means of digital computer programs. It is intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier.
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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