Work

Implementing the Streamline Curvature Method For Preliminary Design of Multi-Stage Axial Compressors

Year: 2024

Type: article

Abstract: The article describes an algorithm for the inverse calculation of a multi-stage axial compressor using the streamline curvature method. Also, using this method, a four-stage axial compressor with a pressure ratio of 3.2 was designed. In addition, a numerical simulation of the flow in this compressor was performed, the results of the numerical simulation were compared with the design parameters, and an analysis of the reasons for the deviation of the parameters from the design parameters was performed. Recommendations for improving the calculation methodology are given.

Source: International Journal of New Findings in Engineering Science and Technology

DOI: 10.61150/ijonfest.2024020204

Author: Hadi Genceli

Institution: Yıldız Technical University

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: bronze

OpenAlex ID: W4402922131

FWCI: 0.178

Cites:

Cited by: 1

Related to: 10