Path: ACPro/ACEngine
% Definitions of data. If no output arguments are specified it will
produce a tab delimited table. If no input and no output arguments
are given it will output a list of all inputs for all of the
available engines. type is the analysis type.
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Form:
def = JetEngineDefinitions( type, engine )
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Inputs
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typeIn (1,:) 'performance' or 'analysis'
engineIn (1,:) 'Ramjet', 'Turbojet', 'Single Spool Turbojet',
'Dual Exhaust Turbofan', 'Mixed Flow Turbofan',
'Turboprop'
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Outputs
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def (:) Definition data structure
.type (1,:) Type
.engine (1,:) Engine
.p p parameters {name description units mks units english}
.d d parameters {name description units mks units english}
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