Design and Optimization Radial Gas Turbine Blade

§ Faculty of Mechanical Engineering Shri Rawatpura Sar...

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Design and Optimization Radial Gas Turbine Blade

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Abstract

The combustion chamber of an automobile gas-turbine engine can be designed to produce a gas temperature distribution at the inlet of the turbine increasing from blade root to blade tip. It is shown in the paper, by means of comparative calculations, that by using such distributions of temperatures blade life can be substantially increased, or else, un expensive materials can be used. Such gas temperature distributions produce non-isentropic flow conditions. It is developed in the paper a method for the aerodynamic design of blades within a non-isentropic flow and it is also shown that if the blades are designed by taking an average gas temperature, as it is usually made, important errors are introduced in the resulting shape of the blade, which reduces the efficiency of the turbine.

References

6 Cites in Article
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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Rahul Mishra, Yogesh Kushwaha, Praveen Singh. 2013. "Design and Optimization Radial Gas Turbine Blade". Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 13 (GJRE Volume 13 Issue 27 (A7)).

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords
Classification
GJRE-A Classification FOR Code: 091399
Version of record

v1.2

Issue date
July 1, 2013

Language
English
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Design and Optimization Radial Gas Turbine Blade

Rahul Mishra
Rahul Mishra
Yogesh Kushwaha
Yogesh Kushwaha
Praveen Singh
Praveen Singh