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- W165156731 abstract "A one-dimensional, dynamic gas turbine engine performance analysis program, based on a modified parallel compressor theory, was enhanced with an added capability to calculate compressor stage characteristics given basic blade correlations, blade and casing geometry, and flow conditions. Total pressure ratio and total temperature ratio across rotors and stators had previously been provided solely by stage characteristics maps created using experimental data or computational means. The user now has the option to have those ratios, or characteristics, calculated via a one-dimensional code during the simulation. Experimental data is still required for calibration of this characteristics prediction code. An existing characteristics prediction code was integrated as a subroutine of the performance analysis program. With flow conditions at the stage inlet and basic stage geometry information provided, the characteristics prediction code calculates the desired ratios and feeds them back to the analysis code. The performance analysis program interacts with the characteristic prediction code whenever rotor or stator performance is required, so it can be run in a steady state or dynamic condition, with or without parallel compressor segments. The performance analysis code, called DYNTECC, operates on a modified parallel compressor theory. The modifications allow it to simulate radial and circumferential mass redistribution, as well as radial work redistribution between the parallel flow segments. These, in turn, make it possible to model the effects of radial and circumferential inlet flow distortion on overall compressor performance. The interface" @default.
- W165156731 created "2016-06-24" @default.
- W165156731 creator A5017475648 @default.
- W165156731 date "2003-01-01" @default.
- W165156731 modified "2023-09-25" @default.
- W165156731 title "Modification of a One-Dimensional Dynamic Compression System Model To Calculate Stage Characteristics Internally" @default.
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