News Help Institutional access
Back to results
Bibliographic record · Consultation and access
Artículo de revista

AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL

C M Vigneswaran et al · Embry-Riddle Aeronautical University · 2021

Open access available
Quick overview. Review the resource’s basic details, then access the content using the main button. This page shows only the information needed to identify, cite, and open the work.
Author / responsible party
C M Vigneswaran et al
Publisher
Embry-Riddle Aeronautical University
Year
2021
ISSN
2374-6793
ISSN
2374-6793
Language
English
Serial publication

3D Printing Technology in Aerospace Industry – A Review

This serial publication contains 428 related contents.
View contents

Resource access

Open the content from the main option or choose another available source.

DOAJ DOAJ Articles
Entrar por DOAJ
Main access

Open access available

Recurso identificado como acceso abierto, sin confirmar automáticamente si es texto completo directo.
Open resource

Summary

Descripción general del contenido del recurso.

<p>The work in this paper aims to increase the maximum lift coefficient of the airfoil by implementing the co-flow jet concept on NACA 0018 airfoil and also to investigate the performance of co-flow jet (CFJ) airfoil. To conduct numerical solution, RANS equations have been solved for 2D incompressible and unsteady flow using the Spalart-Allmaras turbulence model. The suction surface of the airfoil is modified by placing the injection slot near the leading edge and the suction slot near the trailing edge. A small mass of air is withdrawn into the airfoil suction slot, pressurized by a pumping system located inside the airfoil, and re-injecting into the injection slot tangentially to the main stream flow. The CFJ airfoil is enhancing the aerodynamic lift coefficient significantly compare to the baseline airfoil. And also, the numerical analysis is carried out to investigate the effect of the location of injection and suction slot. And it is observed that the aerodynamic lift coefficient of CFJ airfoil is increasing with varying the injection slot away from the leading edge.</p>

How to cite

Elegí el formato que necesitás y copiá la referencia al portapapeles.

APA 7

al, C. M. V. E. (2021). AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL. https://doi.org/10.15394/ijaaa.2021.1555

MLA

al, C M Vigneswaran et. "AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL." 2021. https://doi.org/10.15394/ijaaa.2021.1555.

Chicago

al, C M Vigneswaran et. 2021. "AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL.". https://doi.org/10.15394/ijaaa.2021.1555.

Harvard

al, C. M. V. E. 2021, AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL, Embry-Riddle Aeronautical University, available at: https://doi.org/10.15394/ijaaa.2021.1555 [Accessed 8 Aug. 2026].

Share and print

Save the record, copy its permanent link, or print it as a PDF.

Export reference

You can export the record in common formats for use in a reference manager.

RIS BibTeX

Resource details

Bibliographic information to help confirm that this is the correct material.

Title
AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL
Author / contributors
C M Vigneswaran et al
Publisher
Embry-Riddle Aeronautical University
Publication year
2021
ISSN
2374-6793
ISSN
2374-6793
Language
English

Subjects

Explore related resources through these subjects.

Aerodynamics and Fluid Mechanics
Copied