Aeroelastic tailoring of oscillating supersonic wing with external stores

QR Code

Aeroelastic tailoring of oscillating supersonic wing with external stores

This paper presents aeroelastic tailoring optimization of a swept back supersonic wing with external stores using composite structure material for the wing skin. The analysis has been conducted to calculate the flutter speeds at several altitudes ranging from a negative altitude of -7,943 ft until...

Full description

Bibliographic Details
Main Authors:	Abdullah, Nur Azam, Sulaeman, Erwin
Format:	Article
Language:	English English
Published:	Trans Tech Publications Ltd., Switzerland 2014
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/46477/ http://irep.iium.edu.my/46477/1/AMM.464.110.pdf http://irep.iium.edu.my/46477/4/46477_Aeroelastic%20tailoring%20of%20oscillating_SCOPUS.pdf

Similar Items

Aeroelastic flutter analysis of supersonic wing with multiple external stores
by: Abdullah, Nur Azam, et al.
Published: (2014)

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

Flutter analysis of supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2013)

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

Approximate function for unsteady aerodynamic kernel function of aeroelastic lifting surfaces
by: Sulaeman, Erwin, et al.
Published: (2014)

Supersonic similitude for oscillating non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)

Estimation of stability derivatives in pitch for an oscillating 2-D wedge in supersonic Flow
by: Pavithra, Shanbhag,, et al.
Published: (2016)

Alternate approximate function for kernel function of oscillating lifting surfaces
by: Sulaeman, Erwin, et al.
Published: (2013)

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

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

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

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

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)

CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
by: Munshi, Adnan, et al.
Published: (2018)

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

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

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

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

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

Active control of base pressure in supersonic regime
by: Khan, Sher Afghan, et al.
Published: (2006)

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

CFD analysis of the supersonic nozzle flow with sudden expansion
by: Ahmed, Khizar Pathan, et al.
Published: (2016)

Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2018)

On the evaluation of negative altitude requirement for flutter speed boundary of transport aircraft and UAV
by: Sulaeman, Erwin
Published: (2012)

Accurate geometric stiffness matrix formulation of beam finite element
by: Sulaeman, Erwin
Published: (2011)

Axial stiffness matrix of non-uniform Bernoulli-Euler bar element
by: Sulaeman, Erwin
Published: (2011)

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

Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
by: Pathan, Khizer Ahmed, et al.
Published: (2018)

Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number
by: Khan, Sher Afghan, et al.
Published: (2019)

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

Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM
by: Wirawan, Nanda, et al.
Published: (2018)

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

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

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

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)

Prediction of base pressure in a suddenly expanded flow the processes at supersonic Mach Number Regimes using ANN and CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2020)

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

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

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