Design of turbomachinery blading in transonic flows by the circulation method

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Abstract

The newly developed three-dimensional design technique for turbomachinery blading based on the circulation method has been successfully extended into the transonic flow regime. The main task involves replacing the classical Fourier series expansion technique by a finite-volume method. Calculations were carried out for the design of infinitely thin cascaded blades in transonic flows, including shocked and shockfree cascaded blades.

Original languageEnglish (US)
Pages (from-to)141-146
Number of pages6
JournalJournal of Turbomachinery
Volume114
Issue number1
DOIs
StatePublished - Jan 1992

ASJC Scopus subject areas

  • Mechanical Engineering

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