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

Standard:
Revised:
  • 1999-03-01
 
  • HISTORICAL Access the latest revision: AS681K
Publisher:
  • SAE International
Pages:
30
Scope:

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.

History:
Standard Published Revision Status
AS681K 2016-06-06 Latest Revised
2008-06-12 Historical Revised
1999-03-01 Historical Revised
1996-09-01 Historical Revised
1991-10-28 Historical Revised
1982-10-01 Historical Revised
1982-10-01 Historical Revised
1974-04-15 Historical Revised
AKA:
  • SAE AS 681
Sector:
Topic:
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