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GSP 11 Components
| GSP component blocks |
| GSP 11 introduces a new concept in evaluating the modelling software. Rather than having a crippled version, the GSP 11 LE is fully functional. The only drawback of the LE is that the input data entered in the data entry window is not stored on saving the project. Below the components are listed that can be saved (free) or cannot be saved (licensed). Using this concept every user is free to try the full capabilities of GSP. |
| Gas Path and Multi In/Out Component Library (free, saving in LE enabled) |
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| Control Component Library (free, saving in LE enabled) |
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calculates free state fuel flow by specifying the rotor speed calculates free state fuel flow by specifying the thrust of the cycle |
| Licensed Components (free to evaluate, saving in LE disabled) |
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splits the flow into two separate flows define a custom fluid that enters the gas turbine divide the combustor in segments heat soakage and heat capacity are taken into account model the back pressure as a result of a boiler in the exhaust cools the (compressed) fluid fixed pitch propeller, constant speed propeller controls the splitting of the flow splitter controls the pressure and temperature of the pressure vessel controls the amount of coolant in the intercooler component mixes two types of user specified composition fuels controls the pressure at the end of the back pressure exhaust component schedule the bleed air as function of corrected rotor speed creates a set of ambient conditions to represent the flight envelope of a certain engine calculate design point sweeps for selected parameters control engine based on user specified equation (output parameter or component property parameter) control engine based on user specified equation using a 1-D look-up table control engine based on user specified equation using a map This powerfull schedule control component contains functionality of last 3 schedule control components. generic engine power control component revision of PLA controlled after burner control now containg many more options to control AB define limits to limit certain engine parameters directly modify engine parameters during calculation incorporate design point iteration in your engine model incorporate installation effects in your engine model manage your input for a case model from 1 single component (design, design series, steady state and st. st. series) Define constant expressions to be used in other equations and controllers Define additional custom output expressions |
| STOVL Component Library (not yet released) |
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| Additional Components / Libraries (examples of custom developed libraries) |
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More components have been developed over the years to assist in gas turbine modeling of specific applications, e.g.:
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