Constant Pitch Propeller Design for Low Subsonic Airplane

Constant Pitch Propeller Design for Low Subsonic Airplane

Arif Ahmed Sohel

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Md. Abdus Shamir Talukder

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Dr. Mohammad Arif Hasan Mamun

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1 Bangladesh University of Engineering & Technology (BUET), Dhaka

GJRE Volume 14 Issue A6

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The objective of our study was to evaluate, in a population of Togolese People Living With HIV(PLWHIV), the agreement between three scores derived from the general population namely the Framingham score, the Systematic Coronary Risk Evaluation (SCORE), the evaluation of the cardiovascular risk (CVR) according to the World Health Organization.

Constant pitch propeller whose blade angle is fixed with respect to hub is suitable for low speed airplane. The objectives of this thesis are to determine thrust, torque and the performance of the low subsonic airplane propeller. The thesis has been carried out by the two different approaches-Analytical and Computational Fluid Dynamic (CFD) simulation. The Analytical Method using “Propeller Blade Element Theory” is one of the most effective methodologies available for determining the thrust and torque produced by the propeller. On the other hand, the Computational Fluid Dynamic simulation has been used to simulate and capture the performance of the propeller. Through both methodologies, the propeller performance was analyzed and compared. The results obtained were tabulated and the corresponding graphs were plotted. Both methods suggest that the thrust and torque change with the change in relative velocity. Besides, there are several factors that contribute to the variations in results of the Analytical method and CFD Simulation.

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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.

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Not applicable for this article.

Arif Ahmed Sohel. 2014. \u201cConstant Pitch Propeller Design for Low Subsonic Airplane\u201d. Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 14 (GJRE Volume 14 Issue A6): .

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GJRE Volume 14 Issue A6
Pg. 9- 17

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords

advance ratio airfoil blade element theory CFD coefficients of thrust constant pitch etc Power torque

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Submission ReceivedDecember 13, 2013
RevisedDecember 13, 2013
Peer Review Double Blind
Handling Editor
Accepted December 31, 2013
Published January 15, 2014

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v1.2

Issue date

August 20, 2014

Language

English

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Article Matrices

Total Score: 108

Country: Bangladesh

Subject: Global Journal of Research in Engineering - A : Mechanical & Mechanics

Authors: Arif Ahmed Sohel, Md. Abdus Shamir Talukder, Dr. Mohammad Arif Hasan Mamun (PhD/Dr. count: 1)

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