SAE AIR1419B
Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines.
Standard:
AKA:
- AIR1419
- Revision: B
- 2013-05-28
- S-16 Turbine Engine Inlet Flow Distortion Committee
This document addresses many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability. It provides a review of the development of techniques used to assess engine stability margins in the presence of inlet total-pressure distortion. Specific performance and stability issues that are covered by this document include total-pressure recovery and turbulence effects and steady and dynamic inlet total-pressure distortion.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AIR1419B | 2013-05-28 | Latest | |
| AIR1419A | 1999-03-01 | Historical | |
| AIR1419 | 1983-05-01 | Historical |
- SAE AIR 1419
- Aerospace
- Simulation and Modeling
- Gas turbines