Browse Standards AS681H
Historical REVISED 1999-03-01

Gas Turbine Engine Steady-State and Transient Performance Presentation for Digital Computer Programs AS681H

This Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady-state and transient performance calculated using digital computer programs. It also provides for the presentation of parametric gas turbine data including performance, weight and dimensions computed by digital 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.
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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