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Applications
GSP is a powerful tool for analysis of effects of ambient and flight
conditions, installation losses, deterioration and malfunctions of control-
and other subsystems on performance.
GSP has been used for a variety of applications of both aircraft and
industrial gas turbines.
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Basic applications
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ambient effect analysis,
failure analysis,
deterioration analysis,
fuel type selection,
basic emission calculations,
control system design and diagnostics.
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Advanced applications
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analysis of recuperated turboshaft engine performance,
lift-fan STOVL propulsion systems,
control logic validation,
analysis of thermal load calculation for hot section life consumption modelling,
multi-reactor combustor model emission calculations.
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The following gasturbine engines have been modelled:
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Thrust or Power
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Link
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Description
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Aircraft engines
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JT15D
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10 - 15 kN
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PW
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civil medium-bypass turbofan
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TAY60
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61 - 67 kN
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RR
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civil medium-bypass turbofan
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CFM56
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82 - 151 kN
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GE
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civil high-bypass turbofan
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CF6-80
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233 - 282 kN
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GE
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civil high-bypass turbofan
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RB211
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258 - 270 kN
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RR
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civil high-bypass turbofan
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J85
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12 - 22 kN
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GE
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military AB turbojet
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F100PW220
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65 - 110 kN
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PW
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military low-bypass AB turbofan
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F100PW229
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79 - 130 kN
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PW
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military low-bypass AB turbofan
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JSF119 / PW135
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111 - 178 kN
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JSF
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military low-bypass AB turbofan
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PT6A
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1090 - 1940 hp
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PW
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turboshaft
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MTR390
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1275 - 1910 hp
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RR
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turboshaft
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T700
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1500 - 2600 hp
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GE
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turboshaft
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RTM322
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2100 - 3000 hp
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RR
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turboshaft
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PW125
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- 2500 hp
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PW
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turboshaft
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PW127
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- 2750 hp
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PW
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turboshaft
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Industrial engines
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GT10B
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- 34100 hp
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ABB
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industrial turboshaft
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LM2500
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- 33600 hp
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GE
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industrial turboshaft
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GSP
