Logo

SAE AS681 Rev K

Historical Revision

Gas Turbine Engine Performance Presentation for Computer Programs

$125.00

$125.00

$225.00


Sub Total (1 Item(s))

$ 0.00

Estimated Shipping

$ 0.00

Total (Pre-Tax)

$ 0.00


Document Preview Not Available...

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.

SDO SAE: SAE International
Document Number AS681
Publication Date June 6, 2016
Language en - English
Page Count 26
Revision Level K
Supercedes
Committee
Publish Date Document Id Type View
Aug. 21, 2023 AS681L Revision
June 6, 2016 AS681K Revision
June 12, 2008 AS681J Revision
March 1, 1999 AS681H Revision
Sept. 1, 1996 AS681G Revision
Oct. 28, 1991 AS681F Revision
Oct. 1, 1982 AS681E Revision
Oct. 1, 1982 AS681D Revision
April 15, 1974 AS681C Revision