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Propulsion System Tests
标准号:
AIR1419A
标准名称: Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
同源图形
FORMULA 1
FORMULA 2
Alternative Surge Ma
Different Surge Marg
Effect of Surge Line
Methodology Screens
TABLE 1
Stability Assessment
Fan Surge Margin Ass
Typical Surge Margin
Classical Circumfere
Radial and Mixed Scr
Operational Conditio
Inlet and Aircraft C
Engine Component and
Flight Test Conditio
ARP1420 Guidelines f
Data Scaling Guideli
Recording Frequencie
Analog Tape Informat
Digital Tape Informa
Stability Assessment
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