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Analog Tape Information
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
Propulsion System Te
Flight Test Conditio
ARP1420 Guidelines f
Data Scaling Guideli
Recording Frequencie
Digital Tape Informa
Stability Assessment
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Test Burner Informat
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Aircraft T
Typical FADEC Select
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RANDOM UNCERTAINTY L
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Measuremen
RANDOM UNCERTAINTY L
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Measuremen
CLASS 1, CONTINUOUS
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(R) Sealin
CONTINUOUS NON-RIBBE
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CONTINUOUS NON-RIBBE
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