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CYCLE DESIGN PARAMETRIC STUDY GAS TURB SOFT
CYCLE DESIGN PARAMETRIC STUDY GAS TURB SOFT
parabdulla
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Mar 05, 2025
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About This Presentation
CYCLE DESIGN PARAMETRIC STUDY
Size:
8.69 MB
Language:
en
Added:
Mar 05, 2025
Slides:
35 pages
Slide Content
Slide 1
GasTurb 12 –Tutorial 2
CYCLE DESIGN PARAMETRIC STUDYCYCLE DESIGN PARAMETRIC STUDY
Copyright © GasTurb GmbH
Slide 2
GasTurb GasTurb 12 12 Main WindowMain Window
For this tutorial we will consider a
2 Spool Turbofan.
Copyright © GasTurb GmbH
Slide 3
We Need Some We Need Some DataData
Copyright © GasTurb GmbH
Slide 4
Input Data PageInput Data Page
First we run a single cycle
Copyright © GasTurb GmbH
Slide 5
Single Cycle OutputSingle Cycle Output
This is a cycle for a business jet engine.
Cruise flight condition is 11000m @ Mach
0.8. The overall pressure ratio is rather low
(P3/P2=17.33), burner exit temperature is
1450K and the bypass ratio is 6.
Copyright © GasTurb GmbH
Slide 6
Turbofan Station DesignationTurbofan Station Designation
These are the locations of the thermodynamic
stations and the secondary air system paths
Copyright © GasTurb GmbH
Slide 7
Parametric StudyParametric Study
Now we go for a Parametricstudy.
Copyright © GasTurb GmbH
Slide 8
Parameter SelectionParameter Selection
Click here to run all
cases
This is the HP Compressor Pressure Ratioof
the Single Cyclecalculated before this
parametric study.
Choose a property from the list, double click or drag it to the
parameter page on the right. You can also click the arrow for
moving a parameter from left to right.
We employ
HP Compressor Pressure Ratio
as the only parameter for now.
Copyright © GasTurb GmbH
Slide 9
Graphical OutputGraphical Output
Picture Picture DefinitionDefinition
The result of a parametric study is presented graphically.The result of a parametric study is presented graphically.
Sp. Fuel Consumptionand Net Thrust
are the default plot parameters.
To employ Overall Pressure Ratio P3/P2
as x-axis, drag it to the box below the schematic picture. Then
click Draw y=f(x)
Copyright © GasTurb GmbH
Slide 10
Single ParameterSingle Parameter
Plot With a Single YPlot With a Single Y--AxisAxis
This black square
marks the Cycle
calculated before
beginning the
Parametric study
We go back to the previous
window and select a new view
(New Picture) of the data created
in the Parametric Study
Copyright © GasTurb GmbH
Slide 11
Single ParameterSingle Parameter
A Plot With Several YA Plot With Several Y--AxesAxes
Select the number of y-
axes first!
We will employ several
y-axes
Drag four parameters to the
respective y-axis boxes. Then
click Draw y=f(x)
Copyright © GasTurb GmbH
Slide 12
Plot With Four YPlot With Four Y--AxesAxes
On each y-axis there is
a different symbol.
This line belongs to the
LPT Pressure Ratio
axis –the symbols on
the line and on the axis
are the same.
Close this window to go
for a new Parametric
study.study.
Copyright © GasTurb GmbH
Slide 13
Parameter SelectionParameter Selection
Adding Adding a Second Parametera Second Parameter
Click this tab for
specifying the
second parameter
Click here to run all
cases
Use these
numbers
Burner Exit TemperatureWe employ Burner Exit Temperature
as the second parameter
This is the Burner Exit Temperatureof the cycle
calculated before this Parametric study.
Copyright © GasTurb GmbH
Slide 14
The Default PlotThe Default Plot
No Contour LinesNo Contour Lines
This little black square
marks the cycle calculated marks the cycle calculated
before beginning the
Parametric study
Next have a look at all
the data from a specific
parameter combination.
Click
Detailed Output
Copyright © GasTurb GmbH
Slide 15
Getting the Detailed Output for any Parameter CombinationGetting the Detailed Output for any Parameter Combination
Now we will add more
information to the
picture. Click
New Picture
SELECT
Double click (in GasTurb) to
select T4=1425and
HPC Pressure Ratio = 9
Copyright © GasTurb GmbH
Slide 16
Contour Parameter SelectionContour Parameter Selection
An option: Click
to sort the
property names
alphabetically
Copyright © GasTurb GmbH
Slide 17
Plot with ContoursPlot with Contours
Copyright © GasTurb GmbH
Slide 18
Editing ContoursEditing Contours
Edit the numbers:
Lowest Contour Value = 0.435
Step Size = 0.005
Click to apply the
new settings
Copyright © GasTurb GmbH
Slide 19
The Customized PlotThe Customized Plot
Let us add now a
design limit for
T45 of 1200 K
to the carpet.
Copyright © GasTurb GmbH
Slide 20
Showing Design LimitsShowing Design Limits
Example: Add a Boundary for T45>1200KExample: Add a Boundary for T45>1200K
Upper or
lower limit
Copyright © GasTurb GmbH
Slide 21
Showing Design LimitsShowing Design Limits
Next we go for
another
New Picture
Copyright © GasTurb GmbH
Slide 22
Specific Fuel Consumption (SFC) as a Function of Specific Fuel Consumption (SFC) as a Function of
HPT Pressure RatioHPT Pressure Ratio
overlapping and the plot is
Sometimes the lines are
overlapping and the plot is
difficult to read
Changing the Layout
resolves this problem
The disadvantage of this plot is that The disadvantage of this plot is that
there is no information about
HPT Pressure Ratio anymore.
To correct for that we add contour
lines for HPT Pressure Ratio.We go for
another
New Picture
Copyright © GasTurb GmbH
Slide 23
Specific Fuel Consumption (SFC) as a Function of Specific Fuel Consumption (SFC) as a Function of
Ideal Ideal Jet Velocity Ratio V18/V8Jet Velocity Ratio V18/V8
HP Compressor Pressure Ratio For each HP Compressor Pressure Ratio the
best SFC is achieved if the Ideal Jet Velocity
Ratio V18/V8 is approximately 0.8. This
relation between the bypass nozzle velocity
V18 and the core nozzle velocity V8 can be V18 and the core nozzle velocity V8 can be
achieved by choosing the right Outer Fan
Pressure Ratio.
In the next parametric study we will iterate
Outer Fan Pressure Ratioin such a way that
the Ideal Jet Velocity Ratio V18/V8is equal to
0.8. Thus all the cycles are optimized for
Specific Fuel Consumption SFC .
Closing this window brings us back to the cycle
design input window
Copyright © GasTurb GmbH
Slide 24
Go for IterationsGo for Iterations
Copyright © GasTurb GmbH
Slide 25
Define the IterationDefine the Iteration
How to define an iteration is shown in the
Single Cycle Tutorial
Copyright © GasTurb GmbH
Slide 26
ReRe--Run the Parametric StudyRun the Parametric Study
Copyright © GasTurb GmbH
Slide 27
No Change in this WindowNo Change in this Window
Copyright © GasTurb GmbH
Slide 28
Outer Fan Pressure Ratio Outer Fan Pressure Ratio is Optimizedis Optimized
Copyright © GasTurb GmbH
Slide 29
GasTurb Copy to Clipboard,GasTurb Copy to Clipboard,
Pasted into Power Point and RePasted into Power Point and Re--SizedSized
Copyright © GasTurb GmbH
Slide 30
DeDe--Activating the IterationActivating the Iteration
Click to de-activate the iteration
again
Now run the
Parametric study
again
Copyright © GasTurb GmbH
Slide 31
Outer Fan Pressure Ratio = Outer Fan Pressure Ratio = 1.81.8
Iteration is DeIteration is De--ActivatedActivated
Adjust the scales to make the
picture comparable to the picture
with the optimized Outer Fan
Pressure Ratio.
Copyright © GasTurb GmbH
Slide 32
Outer Fan Pressure Ratio = 1.8Outer Fan Pressure Ratio = 1.8
Repeat clicking this
button until no parameter
values are shown
Copyright © GasTurb GmbH
Slide 33
Outer Fan Pressure Outer Fan Pressure Ratio = 1.8Ratio = 1.8
Select a color
Copyright © GasTurb GmbH
Slide 34
The Overlay on the ClipboardThe Overlay on the Clipboard
Copyright © GasTurb GmbH
Slide 35
Pasted on the Other PicturePasted on the Other Picture
This slide ends the
Tutorial
This slide ends the
Cycle Design Parametric
Tutorial
Copyright © GasTurb GmbH
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