Aerodynamic design system adapting to three dimensional turbine

Ning Yuan; Zhenjia Zhang; Songtao Wang; Zhonghua Gu; Zhongqi Wang; Guotai Feng

Aerodynamic design system adapting to three dimensional turbine

Ning Yuan^*
, Zhenjia Zhang
, Songtao Wang
, Zhonghua Gu
, Zhongqi Wang
, Guotai Feng

^*Corresponding author for this work

School of Energy Science and Engineering

Harbin Institute of Technology

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

3 Scopus citations

Abstract

A 3-D design system was applied to modern turbine design. The main calculating program of this system was a 3-D mutistage inviscous calculating program with loss model as well as the varying specific heat and cooled-air mixing. The stability of the method in interrow mixing treatment was improved by Rieman solver and lax gene. Profile in 2-D datum plane was made by applying the rational B-spline approximation form. The 3-D blade was mounded using Besier curve. This design system included a loss model system in order to assess the effect of turbine accurately.

Original language	English
Pages (from-to)	1-4
Number of pages	4
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	21
Issue number	2
State	Published - 2000

Cite this

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title = "Aerodynamic design system adapting to three dimensional turbine",

abstract = "A 3-D design system was applied to modern turbine design. The main calculating program of this system was a 3-D mutistage inviscous calculating program with loss model as well as the varying specific heat and cooled-air mixing. The stability of the method in interrow mixing treatment was improved by Rieman solver and lax gene. Profile in 2-D datum plane was made by applying the rational B-spline approximation form. The 3-D blade was mounded using Besier curve. This design system included a loss model system in order to assess the effect of turbine accurately.",

author = "Ning Yuan and Zhenjia Zhang and Songtao Wang and Zhonghua Gu and Zhongqi Wang and Guotai Feng",

year = "2000",

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T1 - Aerodynamic design system adapting to three dimensional turbine

AU - Yuan, Ning

AU - Zhang, Zhenjia

AU - Wang, Songtao

AU - Gu, Zhonghua

AU - Wang, Zhongqi

AU - Feng, Guotai

PY - 2000

Y1 - 2000

N2 - A 3-D design system was applied to modern turbine design. The main calculating program of this system was a 3-D mutistage inviscous calculating program with loss model as well as the varying specific heat and cooled-air mixing. The stability of the method in interrow mixing treatment was improved by Rieman solver and lax gene. Profile in 2-D datum plane was made by applying the rational B-spline approximation form. The 3-D blade was mounded using Besier curve. This design system included a loss model system in order to assess the effect of turbine accurately.

AB - A 3-D design system was applied to modern turbine design. The main calculating program of this system was a 3-D mutistage inviscous calculating program with loss model as well as the varying specific heat and cooled-air mixing. The stability of the method in interrow mixing treatment was improved by Rieman solver and lax gene. Profile in 2-D datum plane was made by applying the rational B-spline approximation form. The 3-D blade was mounded using Besier curve. This design system included a loss model system in order to assess the effect of turbine accurately.

UR - https://www.scopus.com/pages/publications/0033728385

M3 - 文章

AN - SCOPUS:0033728385

SN - 1001-4055

VL - 21

SP - 1

EP - 4

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 2

ER -

Aerodynamic design system adapting to three dimensional turbine

Abstract

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