Search Results

Standard

Aircraft Propulsion System Performance Nomenclature

2022-06-21

CURRENT

AS6502

This SAE Aerospace Standard (AS) provides classical propulsion system performance parameter names for aircraft propulsion systems and their derivatives, and describes the logical framework by which new names can be constructed.

Standard

Aircraft Propulsion System Performance Station Designation and Nomenclature

2009-04-07

HISTORICAL

AS755D

This SAE Aerospace Standard (AS) provides performance station designation and nomenclature systems for aircraft propulsion systems and their derivatives.

Standard

Aircraft Propulsion System Performance Station Designation and Nomenclature

2014-01-03

HISTORICAL

AS755E

This SAE Aerospace Standard (AS) provides performance station designation and nomenclature systems for aircraft propulsion systems and their derivatives.

Standard

Aircraft Propulsion System Performance Station Designation and Nomenclature

1997-12-01

HISTORICAL

AS755C

This SAE Aerospace Standard (AS) provides performance station designation and nomenclature systems for aircraft propulsion systems and their derivatives.

Standard

Real-Time Modeling Methods for Gas Turbine Engine Performance

2022-01-20

CURRENT

AIR4548B

The modeling methodologies addressed in this AIR concentrate on the aerothermal portion of the gas turbine propulsion system. Characteristics of the models, the various algorithms used in them, and system integration issues are also reviewed.

Standard

REAL-TIME MODELING METHODS FOR GAS TURBINE ENGINE PERFORMANCE

1995-12-01

HISTORICAL

AIR4548

The modeling methodologies addressed in this AIR concentrate on the aerothermal portion of the gas turbine propulsion system. Characteristics of the models, the various algorithms used in them, and system integration issues are also reviewed.

Standard

Real-Time Modeling Methods for Gas Turbine Engine Performance

2013-04-02

HISTORICAL

AIR4548A

The modeling methodologies addressed in this AIR concentrate on the aerothermal portion of the gas turbine propulsion system. Characteristics of the models, the various algorithms used in them, and system integration issues are also reviewed.

Standard

Gas Turbine Engine Interface Test Data Reduction Computer Programs

2017-11-21

CURRENT

ARP1210E

This SAE Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to the interface of the engine in the airframe or test facility. This ARP also is intended as a guide for the preparation of such computer programs.