Novità Aiuto Accesso istituzionale
Torna ai risultati
Scheda bibliografica · Consultazione e accesso
Artículo de revista

AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL

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

Accesso aperto disponibile
Lettura rapida. Controlla i dati essenziali della risorsa e accedi al contenuto con il pulsante principale. La scheda mostra solo le informazioni necessarie per identificare, citare e aprire l’opera.
Autore / responsabile
C M Vigneswaran et al
Editore
Embry-Riddle Aeronautical University
Anno
2021
ISSN
2374-6793
ISSN
2374-6793
Lingua
Inglés
Pubblicazione seriale

3D Printing Technology in Aerospace Industry – A Review

Questa pubblicazione seriale contiene 428 contenuti correlati.
Vedi contenuti

Accesso alla risorsa

Apri il contenuto dall’opzione principale o scegli un’altra fonte disponibile.

DOAJ DOAJ Articles
Entrar por DOAJ
Accesso principale

Accesso aperto disponibile

Recurso identificado como acceso abierto, sin confirmar automáticamente si es texto completo directo.
Apri risorsa

Riepilogo

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 A small mass of air is withdrawn into the airfoil suction slot, pressurized by a pumping system located inside the airfoil, and re-injecting into the injection slot tangentially to the main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>

Come citare

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].

Condividi e stampa

Salva la scheda, copia il link permanente o stampala in PDF.

Esporta riferimento

Esporta il record nei formati più comuni per usarlo con un gestore bibliografico.

RIS BibTeX

Dettagli della risorsa

Informazioni bibliografiche utili per verificare che sia il materiale corretto.

Titolo
AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL
Autore / collaboratori
C M Vigneswaran et al
Editore
Embry-Riddle Aeronautical University
Anno di pubblicazione
2021
ISSN
2374-6793
ISSN
2374-6793
Lingua
Inglés

Soggetti

Esplora risorse correlate a partire da questi soggetti.

Aerodynamics and Fluid Mechanics
Copiato