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GAS TURBINE ENGINE STEADY STATE PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS
- Aerospace Standard
- AS681C
- Revised
Sector:
Issuing Committee:
Language:
English
Scope
Steady state engine performance programs discussed in this Standard will be confined to two basic performance categories: preliminary design or specification. Preliminary design programs may vary in scope, but will be representative of the defined engine performance until the engine is defined by a specification. A specification program will accurately represent the engine described by the specification and will identify the appropriate model specification. Normally, the computer program will be the primary source of performance data.
Two additional categories of program are status and data reduction interface programs, which are covered by ARP 1211 and 1210 respectively.
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Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
S-15 Gas Turbine Perf Simulation Nomenclature and Interfaces
Welcome to the SAE S-15, Engine Performance Simulation Nomenclature and Interfaces Forum.
Scope: The committee provides recommendations relative to the information contained in mathematical models of aerospace engines and their derivatives and to the coordination of the interfaces between models suppliers and their users. For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright, and Membership" link in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expresed or information posted in this forum. All information posted becomes the property of SAEReference
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