Fluid-structure interactions of variable span wings in low Reynold flows

QR Code

Fluid-structure interactions of variable span wings in low Reynold flows

Numerical method is one of the method which is applied to study the aerodynamics of static variable span morphing wing and to evaluate flow structure over the wing surface (especially leading edge) at different low reynolds number/flow. The numerical result of lift coefficient vs span increment (pen...

Full description

Bibliographic Details
Main Authors:	Salleh, Hafiz, Saharin, Sanisah, Azmi, Mohammad Hanafi, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Science Publishing CorporationPublisher of International Academic Journals 2018
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/66198/ http://irep.iium.edu.my/66198/1/66198_Fluid-structure%20interactions%20of%20variable.pdf http://irep.iium.edu.my/66198/2/66198_Fluid-structure%20interactions%20of%20variable_SCOPUS.pdf

Similar Items

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

Aerodynamics investigation of delta wing at low Reynold’s number
by: Hamizi, Ilya Bashiera, et al.
Published: (2019)

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

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

Control of nozzle flow in a suddenly expanded duct with micro jets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Effect of mach number in a suddenly expanded flow for area ratio 4.84
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Aeroelastic passive control optimization of supersonic composite wing with external stores
by: Sulaeman, Erwin, et al.
Published: (2017)

Experimental investigation of the base flow from the nozzles with sudden expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)

Effects of micro jets on the flow field of the duct with sudden expansion
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)

Study of feasibility of pulse detonation engine powered by alternative fuels
by: Warimani, Mohammad Salman, et al.
Published: (2019)

Effect of area ratio on base pressure in a suddenly expanded duct for under expanded flow ft mach 1.87
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

A matlab based educational software for the study on the effect of cut-out in aircraft wings
by: Mohammed Riyadh, Miah, et al.
Published: (2018)

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

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

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

Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number
by: Renita, sharon Monis, et al.
Published: (2020)

Oscillating supersonic delta wing with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)

Oscillating supersonic delta wings with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)

Estimation of stability derivatives of a delta wing in hypersonic flow
by: Crasta, Asha, et al.
Published: (2012)

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

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

Modeling and structural analysis of three-dimensional wing
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)

Discrete tonal noise of NACA0015 airfoil at low reynolds number
by: Andan, Amelda Dianne, et al.
Published: (2019)

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

Reynolds averaged navier-stokes flow computation of RAE2822 airfoil using gas-kinetic BGK Scheme
by: Ong, Jiunn Chit, et al.
Published: (2009)

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

Base pressure control by supersonic micro jets in a suddenly expanded nozzle
by: Khan, Sher Afghan, et al.
Published: (2018)

Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field
by: Ashfaq, Syed, et al.
Published: (2014)

Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)

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

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

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

Control of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)

Active control of suddenly expanded flow from under expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)

Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012)

Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
by: Crasta, Asha, et al.
Published: (2013)

Studies on wall pressure flow control by micro jets for high area ratio
by: Ashfaq, Syed, et al.
Published: (2014)

Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2018)

Effect of mach number on wall pressure flow field for area ratio 2.56
by: Ashfaq, Syed, et al.
Published: (2014)

Effect on base pressure in suddenly expanded flows with variable location of microjets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)