Analysis of an NACA 4311 Airfoil for Flying Bike

Analysis of an NACA 4311 Airfoil for Flying Bike

Amit Singh Dhakad

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Pramod Singh

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Arun Singh

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Chhattisgarh Swami Vivekanand Technical University

Analysis of an NACA 4311 Airfoil for Flying Bike

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Analysis of an NACA 4311 Airfoil for Flying Bike Banner

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Abstract

The development of the wing has been always such that it should be able to produce the maximum lift due to the high pressure on the bottom surface and low pressure on the top surface of an airfoil. And these concepts clears that the flow of air/velocity of air will be low on the lower surface and higher on the upper surface of an airfoil. So, due to these differences in pressures and velocity the aerial can produce lift. Here to let fly the Bike in the air the Flat bottomed Airfoil has been chosen and usually the flat bottomed airfoil is called as the Clark Y and this has the feature as Maximum thickness of 11.7% at 28% chord and maximum camber of 3.4% at 42% chord.

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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

Amit Singh Dhakad. 2014. \u201cAnalysis of an NACA 4311 Airfoil for Flying Bike\u201d. Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 14 (GJRE Volume 14 Issue A7).

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GJRE Volume 14 Issue A7

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords

clark Y flat bottomed airfoil javafoil NACA 4311 airfoil

Submission ReceivedDecember 11, 2013
Peer Review Double Blind
Handling Editor
Accepted January 3, 2014
Published January 15, 2014

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v1.2

Issue date

October 31, 2014

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Article Matrices

Total Score: 103

Country: India

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

Authors: Amit Singh Dhakad, Pramod Singh, Arun Singh (PhD/Dr. count: 0)

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Publish Date: 2014 10, Fri

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Total Views: 4616

Total Downloads: 2294

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