Procedure for the Analysis and Evaluation of Gaseous Emissions from Aircraft Engines
Steel, Corrosion Resistant, Sheet, Strip, and Plate, 15Cr - 6.5Ni - 0.75Mo - 0.30Cb - 1.5Cu, Consumable Electrode Melted, Solution Heat Treated, Precipitation Hardenable
Cobalt Alloy, Corrosion and Heat-Resistant, Strip, 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe, Solution Heat Treated, Cold Rolled, and Aged, Vacuum Induction Plus Vacuum Consumable Electrode Melted
Aerospace Series - Quality Management Systems - Nonconformance Data Definition and Documentation
General Agreement on Use of AS1182 in Bar and Wire Specifications
General Agreement on Instrumentation Requirements for Precipitation Heat Treatment
General Agreement AM-M GA AM17-A
Heat Treatment of Titanium and Titanium Alloys Raw Material
Gas Turbine Engine Performance Presentation for Computer Programs
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.