Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)

QR Code

Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)

An experimental investigation has been carried out to evaluate the capabilities of differential spoiler setting (DSS) in modifying the wingspan loading. The particle image velocimetery (PIV) technique was used in a low speed wind tunnel facility to measure wake velocities at four locations downstrea...

Full description

Bibliographic Details
Main Authors:	Elsayed, Omer Ali, Omar, Ashraf Ali E., Asrar, Waqar, Kwon, Kijung
Format:	Article
Language:	English
Published:	Elsevier Masson SAS 2011
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/2094/ http://irep.iium.edu.my/2094/1/Effect_of_differential_spoiler_setting_%28DSS%29_on_thye_wake_vortices_of_a_wing_at_high-lift-configuration_%28HLC%29.pdf

Similar Items

Inﬂuence of differential spoiler settings on the wake vortex characterization and alleviation
by: Elsayed, Omer Ali, et al.
Published: (2010)

Influence of differential spoiler settings on the wake the vortex characterization and alleviation
by: Elsayed, Omer Ali, et al.
Published: (2010)

Evolution of NACA23012 wake vortices structure using PIV
by: Elsayed, Omer Ali, et al.
Published: (2012)

Numerical study of effect of spoiler configuration on wake vortex alleviation
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)

Numerical investigation of the effect of spoilers configuration on wake vortex
by: Omar, Ashraf Ali, et al.
Published: (2012)

Experimental investigation of plain- and flapped-wing tip vortices
by: Elsayed, Omer Ali, et al.
Published: (2009)

Span load modification via differential spoiler setting
by: Elsayed, Omer Ali, et al.
Published: (2010)

Numerical investigation of the vortical flow over delta wing and reverse delta wing
by: Omar, Ashraf Ali E., et al.
Published: (2012)

Numerical investigation of the effect of spoiler’s configuration on wake vortex
by: Omar, Ashraf Ali E., et al.
Published: (2012)

Experimental investigation of wing tip vortex
by: Elsayed, Omer Ali, et al.
Published: (2009)

Induced rolling moment for NACA4412 plain and flapped wing
by: Elsayed, Omer Ali, et al.
Published: (2010)

Investigation of the vortical flow around a reverse delta wing
by: Altaf, Afaq, et al.
Published: (2011)

Experimental investigation of the vortical flow around a reverse delta wing using PIV
by: Altaf, Afaq, et al.
Published: (2010)

Evaluation of aircraft wing-tip vortex using PIV
by: Elsayed, Omer Ali, et al.
Published: (2009)

Numerical investigation of the flow over delta wing and reverse delta wing
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)

Study of the reverse delta wing
by: Altaf, Afaq, et al.
Published: (2011)

Experimental investigation of free wing IIUM-UAV configuration
by: Omar, Ashraf Ali, et al.
Published: (2010)

Aerodynamics of porous airfoils and wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2018)

Wind tunnel testing on a generic model of a hybrid lifting hull
by: UlHaque, Anwar, et al.
Published: (2016)

A review on aerodynamics of nonflapping bird wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)

Conceptual design of a winged hybrid airship
by: UlHaque, Anwar, et al.
Published: (2014)

Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
by: Asrar, Waqar, et al.
Published: (2015)

Impact of a reverse delta type add-on device on the flap-tip vortex of a wing
by: Altaf, Afaq, et al.
Published: (2016)

Effect of a directionally porous wing tip on tip vortex
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2020)

Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Experimental investigation of the influence of a reverse delta type add-on device on the flap-tip vortex of a wing
by: Altaf, Afaq, et al.
Published: (2017)

Comparison of digital DATCOM and wind tunnel data of a winged hybrid airship’s generic model
by: Ul Haque, Anwar, et al.
Published: (2014)

Literature review : Biomimetic and conventional aircraft wing tips
by: Ahmed Siddiqui, Naseeb, et al.
Published: (2017)

Power-off static stability analysis of a clean configuration of a hybrid buoyant aircraft
by: Ul Haque, Anwar, et al.
Published: (2015)

Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
by: Malik, Khurshid, et al.
Published: (2018)

Design and fabrication of a winged hybrid airship model for IIUM-LSWT
by: UlHaque, Anwar, et al.
Published: (2015)

Flow visualization over a circular planform wing
by: Suliman , M. M. Ali, et al.
Published: (2013)

Highly accurate compact flowfield dependent variation method for solving two-dimensional navier-stokes equations
by: Elfagi, Abdulhafid M., et al.
Published: (2011)

Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali, et al.
Published: (2010)

Numerical simulation of a low aspect ratio wing at low Reynolds number
by: Suliman , M. M. Ali, et al.
Published: (2013)

Estimation of aerodynamic parameters of IIUM hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)

Higher order compact-flowfield dependent variation (HOC-FDV) solution of one-dimensional problems
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)

The accuracy of the gas-kinetic BGK finite difference method for solving 3-D compressible inviscid flows
by: Ong, Jiunn Chit, et al.
Published: (2011)

Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012)

Design, fabrication and experimental testing of IIUM free wing unmanned aerial vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali E., et al.
Published: (2011)