Design of turbomachinery blading in transonic flows by the circulation method

T. Q. Dang

doi:10.1115/1.2927977

Design of turbomachinery blading in transonic flows by the circulation method

T. Q. Dang

Department of Mechanical & Aerospace Engineering

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

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 language	English (US)
Pages (from-to)	141-146
Number of pages	6
Journal	Journal of Turbomachinery
Volume	114
Issue number	1
DOIs	https://doi.org/10.1115/1.2927977
State	Published - Jan 1992

ASJC Scopus subject areas

Mechanical Engineering

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10.1115/1.2927977

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title = "Design of turbomachinery blading in transonic flows by the circulation method",

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.",

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AB - 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.

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Design of turbomachinery blading in transonic flows by the circulation method

Abstract

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