NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES

Hamood Ur Rahman; Adnan Maqsood; Rizwan Riaz; Laurent Dala

NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES

Hamood Ur Rahman, Adnan Maqsood^*, Rizwan Riaz, Laurent Dala

^*Corresponding author for this work

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

Abstract

This research aims to find the fundamental effects of high lift devices on the stability characteristics of a high-lift airfoil through computational fluid dynamics. Stability derivatives are calculated for four configurations: clean, slat deployed, flap deployed, and slat and flap deployed configuration. The static and dynamic coefficients are calculated by using the forced oscillation technique. Simulations are performed at various angles of attack and keeping the oscillation amplitude and frequency constant. This approach enabled the efficient and accurate computation of stability derivatives. The results indicate an improvement in static stability characteristics; however, the dynamic stability deteriorates with the deployment of high-lift devices.

Original language	English
Title of host publication	32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
Publisher	International Council of the Aeronautical Sciences
ISBN (Electronic)	9783932182914
Publication status	Published - 2021
Event	32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 - Shanghai, China Duration: 6 Sept 2021 → 10 Sept 2021

Conference

Conference	32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
Country/Territory	China
City	Shanghai
Period	6/09/21 → 10/09/21

Keywords

CFD
High-lift
Pitch moment damping
Stability

Cite this

@inproceedings{b8261ecd432d4ba3adffb1b40c0fb087,

title = "NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES",

abstract = "This research aims to find the fundamental effects of high lift devices on the stability characteristics of a high-lift airfoil through computational fluid dynamics. Stability derivatives are calculated for four configurations: clean, slat deployed, flap deployed, and slat and flap deployed configuration. The static and dynamic coefficients are calculated by using the forced oscillation technique. Simulations are performed at various angles of attack and keeping the oscillation amplitude and frequency constant. This approach enabled the efficient and accurate computation of stability derivatives. The results indicate an improvement in static stability characteristics; however, the dynamic stability deteriorates with the deployment of high-lift devices.",

keywords = "CFD, High-lift, Pitch moment damping, Stability",

author = "\{Ur Rahman\}, Hamood and Adnan Maqsood and Rizwan Riaz and Laurent Dala",

note = "Publisher Copyright: {\textcopyright} 2021 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. All rights reserved.; 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 ; Conference date: 06-09-2021 Through 10-09-2021",

year = "2021",

language = "English",

booktitle = "32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021",

publisher = "International Council of the Aeronautical Sciences",

address = "Germany",

}

Ur Rahman, H, Maqsood, A, Riaz, R & Dala, L 2021, NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES. in 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. International Council of the Aeronautical Sciences, 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021, Shanghai, China, 6/09/21.

NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES. / Ur Rahman, Hamood; Maqsood, Adnan; Riaz, Rizwan et al.
32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. International Council of the Aeronautical Sciences, 2021.

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

TY - GEN

T1 - NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES

AU - Ur Rahman, Hamood

AU - Maqsood, Adnan

AU - Riaz, Rizwan

AU - Dala, Laurent

PY - 2021

Y1 - 2021

N2 - This research aims to find the fundamental effects of high lift devices on the stability characteristics of a high-lift airfoil through computational fluid dynamics. Stability derivatives are calculated for four configurations: clean, slat deployed, flap deployed, and slat and flap deployed configuration. The static and dynamic coefficients are calculated by using the forced oscillation technique. Simulations are performed at various angles of attack and keeping the oscillation amplitude and frequency constant. This approach enabled the efficient and accurate computation of stability derivatives. The results indicate an improvement in static stability characteristics; however, the dynamic stability deteriorates with the deployment of high-lift devices.

AB - This research aims to find the fundamental effects of high lift devices on the stability characteristics of a high-lift airfoil through computational fluid dynamics. Stability derivatives are calculated for four configurations: clean, slat deployed, flap deployed, and slat and flap deployed configuration. The static and dynamic coefficients are calculated by using the forced oscillation technique. Simulations are performed at various angles of attack and keeping the oscillation amplitude and frequency constant. This approach enabled the efficient and accurate computation of stability derivatives. The results indicate an improvement in static stability characteristics; however, the dynamic stability deteriorates with the deployment of high-lift devices.

KW - CFD

KW - High-lift

KW - Pitch moment damping

KW - Stability

UR - https://www.scopus.com/pages/publications/85124486839

M3 - Conference contribution

AN - SCOPUS:85124486839

BT - 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021

PB - International Council of the Aeronautical Sciences

T2 - 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021

Y2 - 6 September 2021 through 10 September 2021

ER -

NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES

Abstract

Conference

Keywords

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