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Fan Surge-Pressure-Ratio Loss Coefficients
标准号:
AIR1419A
标准名称: Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
同源图形
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formula 55
formula 56
formula 57
formula 57
formula 58
formula 59
formula 60
formula 60
formula 61
formula 62
formula 60
formula 61
formula 62
formula 63
formula 64
Turbofan Thrust Loss
formula 65
formula 63
formula 64
Stability Assessment
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