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Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
- Aerospace Standard
- AIR1419B
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
The intent of this document is to provide a basic understanding of the effects of inlet total-pressure distortion on the performance of gas turbine engines, particularly in military applications.
Recommended Content
| Aerospace Standard | Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines |
| Technical Paper | New Generation Engines - The Military Outlook for Adaptive Propulsion Systems |
| Aerospace Standard | Gas Turbine Jet Exhaust Noise Prediction |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE 1 | ALTERNATIVE STABILITY MARGIN DEFINITIONS | |
| TABLE 2 | DIFFERENT STABILITY MARGIN DEFINITIONS RESULT IN DIFFERENT DISTORTION ACCOUNTING | |
| TABLE 3 | EFFECT OF STABILITY LIMIT LINE EXTRAPOLATION ON STABILITY ACCOUNTING | |
| TABLE 4 | METHODOLOGY SCREENS AND COEFFICIENT DETERMINATION | |
| TABLE 5 | STABILITY ASSESSMENT FACTORS | |
| TABLE 6 | FAN STABILITY-PRESSURE-RATIO LOSS COEFFICIENTS | |
| TABLE 7 | FAN STABILITY MARGIN ASSESSMENT | |
| TABLE 8 | TYPICAL STABILITY MARGIN ASSESSMENT | |
| TABLE 9 | CLASSICAL CIRCUMFERENTIAL SCREENS | |
| TABLE 10 | RADIAL AND MIXED SCREENS | |
| TABLE 11 | OPERATIONAL CONDITIONS | |
| TABLE 12 | TURBOFAN THRUST LOSS SYNTHESIS | |
| TABLE 13 | INLET AND AIRCRAFT COMPONENT TESTS | |
| TABLE 14 | ENGINE COMPONENT AND ENGINE TESTS | |
| TABLE 15 | PROPULSION SYSTEM TESTS | |
| TABLE 16 | FLIGHT TEST CONDITIONS | |
| TABLE 17 | ARP1420 GUIDELINES FOR LOCATION OF THE AIP | |
| TABLE 18 | DATA SCALING GUIDELINES: STROUHAL NUMBER CONSTANT (SAME REYNOLDS NUMBER AND MACH NUMBER) |
Issuing Committee
S-16 Turbine Engine Inlet Flow Distortion Committee
Scope: Committee S-16 develops uniform procedures for adoption by industry. These procedures will permit representation of inlet distortion and evaluation of its effect on propulsion systems' stability and performance.
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