Path: Thermal/Brayton
% Designs a centrifugal compressor.
Type CentrifugalCompressor for a demo from the reference.
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Form:
CentrifugalCompressor; % demo
d = CentrifugalCompressor; % data structure
d = CentrifugalCompressor( d )
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Inputs
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d (.) Input data structure
.d2 (1,1) Outlet diameter of the impeller
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Outputs
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d (.) Augmented data structure
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Reference: Mattingly, Jack D. ,"Elements of Gas Turbine Propulsion,"
McGraw Hill, 1996, pp 677-683.
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ACPro: ACEngine/MachFromMassFlowParameter ACPro: ACEngine/MassFlowParameter SC: Environs/MolWt2R Common: General/DisplayLatexTable
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