The Effect of Supersonic Flows on Different Profiles of Aircraft Wings

The Effect of Supersonic Flows on Different Profiles of Aircraft Wings

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Ahmed Soliman M.Sherif

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Novosibirsk State Technical University

The Effect of Supersonic Flows on Different Profiles of Aircraft Wings

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Abstract

When a supersonic stream flows around a thin profile, the pressure acting on the surface element does not depend on the shape of the rest of the profile, but depends only on the slope of the element itself, that is, on the local angle of attack. The local angle of attack is the angle between the surface element and the velocity vector of the undisturbed flow Coefficient of pressure.

References

9 Cites in Article

Reference Format

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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

Ahmed Soliman M.Sherif. 2017. \u201cThe Effect of Supersonic Flows on Different Profiles of Aircraft Wings\u201d. Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 17 (GJRE Volume 17 Issue A2): .

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GJRE Volume 17 Issue A2
Pg. 9- 26

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords

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Classification

GJRE-A Classification: FOR Code: 120499

Submission ReceivedDecember 9, 2016
Peer Review Double Blind
Handling Editor
Accepted December 31, 2016
Published January 15, 2017

Version of record

v1.2

Issue date

July 31, 2017

Language

en

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Article Matrices

Total Score: 101

Country: Unknown

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

Authors: Ahmed Soliman M.Sherif (PhD/Dr. count: 0)

View Count (all-time): 244

Total Views (Real + Logic): 3596

Total Downloads (simulated): 1780

Publish Date: 2017 07, Mon

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Total Views: 3596

Total Downloads: 1780

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Published Article

When a supersonic stream flows around a thin profile, the pressure acting on the surface element does not depend on the shape of the rest of the profile, but depends only on the slope of the element itself, that is, on the local angle of attack. The local angle of attack is the angle between the surface element and the velocity vector of the undisturbed flow Coefficient of pressure.

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