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Aircraft Gas Turbine Engine Design Principles by RUSxALI 77 is a document available to read on EtoBox.

What is Aircraft Gas Turbine Engine Design Principles about?

The document presents proceedings from the RTO AVT Symposium on aircraft gas turbine engine design, focusing on the development of mathematical models for multi-stage turbomachinery flow analysis. It discusses the average passage flow model and its predictive capabilities, highlighting experimental data from a NASA compressor to assess model accuracy. An erratum is included, correcting the printed version of a specific paper within the proceedings.

Author

RUSxALI 77

Language

EN