Revision B, February 1, 2002
Gas Turbine Engine Inlet Flow Distortion Guidelines
Includes all amendments and changes through Reaffirmation Notice , July 2011
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Revision B, April 2011
CONFIGURATION MANAGEMENT STANDARD * FORMERLY TECHAMERICA -EIA-649
Description / Abstract:
The turbine-engine inlet flow distortion methodology addressed
in this document applies only to the effects of inlet
total-pressure distortion. Practices employed to quantify these
effects continue to develop and, therefore, periodic updates are
anticipated. The effects of other forms of distortion on flow
stability and performance, and of any distortion on aeroelastic
stability are not addressed.