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00_memo.txt
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00_memo.txt
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----------
Author: Tomonobu Aozasa
Date: 2019/10/12
----------
Examples::Engines::
TurboJet001
DesignPoint::
_001
_002
OffDesignSim::
_003
_004
_005
1st transient model runnning successfully, only shaft inertia causes transient response
_006
ClosedVolume added downstream of turbine
_007
_008
_009
_010
_011
_012
TurboFan001
DesignPoint::
_001
design point calc model. Brn036.fluid_2.T input.
_002
design point calc model for parametric study.
user inputs: BPR, tgt-thrust
as calculated: Brn036.fluid_2.T
_004
design point calc model for parametric study.
user inputs: Brn036.fluid_2.T, Trb041.effDes, Trb046.effDes
OffDesignSim::
_003
model for off-design simulaion.
operable
_005
shafts are removed from _003
NOT operable
MSZ006A1_engine001
DesignPoint::
_001
_002
MSZ006A1_engine002
DesignPoint::
_001
_002
----------