A Method for Calculating the Angle of Attack Applicable to the Rotational Speed Range of Tip Speed Ratio Less Than 1 in a Turbine Performance Analysis Model Using Aerodynamic Characteristics

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Published
2025-02-15
DOI
https://doi.org/10.1109/cpeee64598.2025.10987273
Primary Topic
Turbomachinery Performance and Optimization
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article
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article

A Method for Calculating the Angle of Attack Applicable to the Rotational Speed Range of Tip Speed Ratio Less Than 1 in a Turbine Performance Analysis Model Using Aerodynamic Characteristics

Kazuhisa Naoi
Turbomachinery Performance and Optimization
article

A Method for Calculating the Angle of Attack Applicable to the Rotational Speed Range of Tip Speed Ratio Less Than 1 in a Turbine Performance Analysis Model Using Aerodynamic Characteristics

Kazuhisa Naoi
article en

Abstract

No abstract available for this paper.
Nihon University (JP)
Affordable and clean energy
Openalex Percentile: Top 86%
Turbomachinery Performance and Optimization
DOISourceOpenAlex
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A Method for Calculating the Angle of Attack Applicable to the Rotational Speed Range of Tip Speed Ratio Less Than 1 in a Turbine Performance Analysis Model Using Aerodynamic Characteristics — Kazuhisa Naoi · (2025) | TGRS Research Map | TGRS