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Behavior of Key Performance Parametersand Temperatures During a Rapid ThrottleTransient for a Typical Turbine Engine at M = 1.0 at 36,000 ft
标准号：
AIR5020
标准名称： Time-Dependent In-Flight Thrust Determination
同源图形
Station Numbering Sy
Force Components for
Airplane Schematic I
Time-DependentThrust
Time-DependentThrust
Threshold Transient
Acceptable Attitude
Typical Gas-Path Noz
Real-Time Thrust Met
Flow Chart of the SG
ExampleofCalculation
ExampelofCalculation
Validation of Transi
Validation and Refin
Transient Simulation
Errors in Gas Path M
Validation of Transi
Typical Ground-Level
Altitude Test Facili
Altitude Test Facili
Results for 1-min Sw
Comparison of Engine
Transient Effects on
Airjet Distortion Ge
IRT Thrust Response
Thrust Response Comp
Thrust Overshoot
Thrust Droop
Thrust Vector Respon
Typical Aircraft Tie
AEDC Tunnel 16T Unce
Features of a Flight
Typical Flight Instr
Instrumentation Syst
Example of a Real-Ti
Typical Gas Path Met
Thrust Stand Force B
Multi-Axis Thrust St
Inlet Duct Mass Capa
Mach Probe
Mach Probe Calibrati
formula 20
Example of a Thrust
Aircraft Force Balan
Example Aircraft Acc
Example Push-Over/Pu
Example Fixed-Thrott
Example Variable-Thr
Vehicle Drag Poles -
Vehicle Drag Polar -
Vehicle Drag Polar -
Vehicle Drag Polar -
Vehicle Drag Polars
Vehicle Drag Polar f
Angle of Attack Effe
Maneuver Effects on
Horizontal Tail Lift
Airflow Hysteresis E
Comparison of Thrott
Aircraft Flight Cond
Engine and Aircraft
Throttle Transient T
Comparison of F|PFan
Max to IRT to Idle
P L F to Max
Comparison of Variou
Problems With Fuel F
Comparison of Variou
Throttle Frequency S
Typical Throttle Inp
Flight Conditions
Throttle Frequency S
Comparison of Left E
F ipf, f/w t
Frequency Response o
Frequency Response o
FIGURE A1
FIGURE A2
FIGURE A3
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