Numerical analysis of FDV method for one-dimensional Euler equations

QR Code

Numerical analysis of FDV method for one-dimensional Euler equations

Finite volume form of Flowfield Dependent Variation (FDV) method was implemented into upwind scheme in order to solve one-dimensional Euler equations. The implementation of FDV method was motivated by its ability in solving the transition and interaction between different flow regimes based on the s...

Full description

Bibliographic Details
Main Authors:	Bin Zulkafli, Mohd Fadhli, Omar, Ashraf Ali E., Asrar, Waqar
Format:	Proceeding Paper
Language:	English
Published:	2012
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/26781/ http://irep.iium.edu.my/26781/1/ICMAE2012-fadhli-v2.pdf

Similar Items

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

A high order compact-flowfield dependent variation (HOC-FDV)method for inviscid flows
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)

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

Arbitrary Lagrangian-Eulerian Form of Flowfield Dependent Variation (ALE-FDV) Method for 3D Problems
by: Zulkifli, Mohammad, et al.
Published: (2014)

Higher order compact-flowfield dependent variation (HOCFDV) method for solving navier-stokes equations
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)

Flowfield dependent variation method for one dimensional stationary and moving boundary problems
by: Zulkifli, Mohammad, 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)

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

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

A gas-kinetic BGK solver for two-dimensional turbulent compressible flow
by: Ong, Jiunn Chit, et al.
Published: (2008)

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

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)

Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
by: Mawlood, M.K., et al.
Published: (2006)

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

Study of the 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)

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

Flowfield-dependent variation method for moving-boundary problems
by: Fadhli, Mohammad, et al.
Published: (2015)

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

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

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

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

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

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

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

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)

Effect of diamond shaped strut with cylindrical pitch rod in subsonic wind tunnel testing
by: UlHaque, Anwar, et al.
Published: (2017)

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

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

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)

Arbitrary lagrangian-eulerian form of flowfield dependent variation method for moving boundary problems
by: Zulkifli, Mohd fadhli, et al.
Published: (2014)

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

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

Hypersonic flow simulation by the gas-kinetic bhatnagar-gross-krook scheme
by: Chit, O.J., et al.
Published: (2005)

The Efficiency of Gas-Kinetic BGK scheme for solving 2-d compressible inviscid regular shock reflection problem
by: Ong, Jiunn Chit, et al.
Published: (2004)

A BGK-based two-equation turbulence model algorithm for solving compressible navier-stokes equations
by: Ong, Jiunn Chit, et al.
Published: (2013)

Computation Of 2d Inviscid Compressible Flow Using An Entropy Consistent Euler Flux
by: Roslan, Nur Khairunnisa Hanisah
Published: (2013)

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)