封面图片

Induced rolling moment for NACA4412 plain and flapped wing

Purpose – The paper aims to compute rolling moments on a follower aircraft wing due to vortices generated by a plain and flapped NACA4412 wing using experimental particle image velocimetery (PIV) data. Design/methodology/approach – This paper describes the detailed variation of the induced rolli...

Saved in:

书目详细资料
Main Authors:	Elsayed, Omer Ali, Kwon, Kijung, Asrar, Waqar, Omar, Ashraf Ali E.
格式:	Article
语言:	English
出版:	Emerald Group Publications Limited 2010
主题:	TL500 Aeronautics
在线阅读:	http://irep.iium.edu.my/1969/1/Induced_rolling%5B1%5D.pdf http://irep.iium.edu.my/1969/ http://www.emeraldinsight.com/journals.htm?issn=0002-2667&volume=82&issue=1&articleid=1840379&show=abstract
标签:	添加标签没有标签, 成为第一个标记此记录!

相似书籍

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

Effects of bio-inspired surface roughness on a swept back tapered NACA 4412 wing
由: Malik, Khurshid, et al.
出版: (2019)

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

Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)
由: Elsayed, Omer Ali, et al.
出版: (2011)

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

Vortex formation in unsteady flow over NACA 4412 and NACA 4424 airfoils
由: Hadi, Muhammad Irfan, et al.
出版: (2020)

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

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

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

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

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

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

Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow
由: Crasta, Asha, et al.
出版: (2016)

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

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

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

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

Laminar separation bubble and flow topology of NACA 0015 at low reynolds number
由: Hassan, Mohamed Ibren, et al.
出版: (2021)

Stability and takeoff ground roll issues of hybrid buoyant aircraft
由: UlHaque, Anwar, et al.
出版: (2014)

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

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

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

Roll control reversal of variable swept wing in supersonic flow
由: Ibren, Mohamed, et al.
出版: (2019)

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

Numerical prediction of trailing edge noise at low Reynolds number with modified trailing edges of a NACA 0015 airfoil
由: Hassan, Mohamed Ibren, et al.
出版: (2024)

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

Experimental Investigation of Low Reynolds Number Flow Around a Serrated NACA 0015 Airfoil
由: Hassan, Mohamed Ibren, et al.
出版: (2023)

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

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

Large Eddy simulation of low Reynolds number flow around a NACA0015 airfoil with modified trailing edges
由: Hassan, Mohamed Ibren, et al.
出版: (2023)

Effect of roll angle configurations of a reverse delta type add-on device on wing tip vortex alleviation
由: Altaf, Afaq, et al.
出版: (2024)

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

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

Vortex Lattice Simulations of Attached and Separated Flows around Flapping Wings
由: Thomas, Lambert, et al.
出版: (2017)

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

Pitch and roll derivatives of a delta wing with curved leading edge in high speed flow
由: Ghosh, K, et al.
出版: (1990)

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

CFD Simulation of NACA 2412 airfoil with new cavity shapes
由: Samuel, Merryisha, et al.
出版: (2022)

Experimental study on the effect of boundary layer control on the aerodynamics characteristics of NACA 0021 Aerofoil
由: Syed Mohamed Ali, Jaffar, et al.
出版: (2021)

Effect of external acoustic excitation on NACA0015 discrete tonal noise
由: Andan, Amelda Dianne, et al.
出版: (2018)