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Author: Tomonobu Aozasa
Date: 2019/10/12
		
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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
			
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