On the effects of discrete and continuous vortex-gust encounters

Berk Zaloglu; Murat Saritas; Oksan Cetiner; Albert Medina; Arif Cem Gözükara

doi:10.2514/6.2020-0554

On the effects of discrete and continuous vortex-gust encounters

Berk Zaloglu, Murat Saritas, Oksan Cetiner, Albert Medina, Arif Cem Gözükara

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

4 Citations (Scopus)

Abstract

In this study the aerodynamic response of wings encountering vortex gusts have been investigated using experimental and computational methods. Effects of different gust parameters on wing loading are investigated for periodic vortex gusts encountering a NACA0012 wing at various angles of attack. Presented experimental results are from two different facilities and together with the computational results provide in agreement an insight into the underlying flow physics of vortex-gust encounters. On the other hand, although there are major differences between experimental and computational conditions for transient vortex gust encounter case, including wing shape, Reynolds number and gust parameters, the scaling puts forward the typical gust response.

Original language	English
Title of host publication	AIAA Scitech 2020 Forum
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624105951
DOIs	https://doi.org/10.2514/6.2020-0554
Publication status	Published - 2020
Event	AIAA Scitech Forum, 2020 - Orlando, United States Duration: 6 Jan 2020 → 10 Jan 2020

Publication series

Name	AIAA Scitech 2020 Forum
Volume	1 PartF

Conference

Conference	AIAA Scitech Forum, 2020
Country/Territory	United States
City	Orlando
Period	6/01/20 → 10/01/20

Bibliographical note

Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Access to Document

10.2514/6.2020-0554

Cite this

@inproceedings{a00c53df862544288e17ba85e0425b68,

title = "On the effects of discrete and continuous vortex-gust encounters",

abstract = "In this study the aerodynamic response of wings encountering vortex gusts have been investigated using experimental and computational methods. Effects of different gust parameters on wing loading are investigated for periodic vortex gusts encountering a NACA0012 wing at various angles of attack. Presented experimental results are from two different facilities and together with the computational results provide in agreement an insight into the underlying flow physics of vortex-gust encounters. On the other hand, although there are major differences between experimental and computational conditions for transient vortex gust encounter case, including wing shape, Reynolds number and gust parameters, the scaling puts forward the typical gust response.",

author = "Berk Zaloglu and Murat Saritas and Oksan Cetiner and Albert Medina and G{\"o}z{\"u}kara, {Arif Cem}",

note = "Publisher Copyright: {\textcopyright} 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Scitech Forum, 2020 ; Conference date: 06-01-2020 Through 10-01-2020",

year = "2020",

doi = "10.2514/6.2020-0554",

language = "English",

isbn = "9781624105951",

series = "AIAA Scitech 2020 Forum",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "AIAA Scitech 2020 Forum",

}

TY - GEN

T1 - On the effects of discrete and continuous vortex-gust encounters

AU - Zaloglu, Berk

AU - Saritas, Murat

AU - Cetiner, Oksan

AU - Medina, Albert

AU - Gözükara, Arif Cem

PY - 2020

Y1 - 2020

N2 - In this study the aerodynamic response of wings encountering vortex gusts have been investigated using experimental and computational methods. Effects of different gust parameters on wing loading are investigated for periodic vortex gusts encountering a NACA0012 wing at various angles of attack. Presented experimental results are from two different facilities and together with the computational results provide in agreement an insight into the underlying flow physics of vortex-gust encounters. On the other hand, although there are major differences between experimental and computational conditions for transient vortex gust encounter case, including wing shape, Reynolds number and gust parameters, the scaling puts forward the typical gust response.

AB - In this study the aerodynamic response of wings encountering vortex gusts have been investigated using experimental and computational methods. Effects of different gust parameters on wing loading are investigated for periodic vortex gusts encountering a NACA0012 wing at various angles of attack. Presented experimental results are from two different facilities and together with the computational results provide in agreement an insight into the underlying flow physics of vortex-gust encounters. On the other hand, although there are major differences between experimental and computational conditions for transient vortex gust encounter case, including wing shape, Reynolds number and gust parameters, the scaling puts forward the typical gust response.

UR - http://www.scopus.com/inward/record.url?scp=85091756204&partnerID=8YFLogxK

U2 - 10.2514/6.2020-0554

DO - 10.2514/6.2020-0554

M3 - Conference contribution

AN - SCOPUS:85091756204

SN - 9781624105951

T3 - AIAA Scitech 2020 Forum

BT - AIAA Scitech 2020 Forum

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - AIAA Scitech Forum, 2020

Y2 - 6 January 2020 through 10 January 2020

ER -

On the effects of discrete and continuous vortex-gust encounters

Abstract

Publication series

Conference

Bibliographical note

Access to Document

Other files and links

Fingerprint

Cite this