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BAMBANG BASUNO
bambangb@uthm.edu.my
View Curriculum Vitae

Note : H-index and Citation are based on current records accessed through the Scopus API.


  • Areas of Research Interest

    • Info!

    Areas of Research Interest Not Found.

  • List of Grant Awarded
    • 01-SEP-22 ~ 31-AUG-24 Q115 : A Novel Approach for the Efficient Prediction of Convection-Diffusion of Water Vapor to Describe the Dynamics of Aircraft Wake Vortex
    Convection-Diffusion; Shishkin-graded; aircraft wake vortex, Universiti, RM 20000

    16-NOV-22 ~ 15-NOV-23 Q253 : The Application Computational Fluid Dynamics for Solving Advection-Diffusion Equation in Incompressible Navier-Stokes Equation Flow Problem
    Advection-diffusion; Incompressible flow, Universiti, RM 15600

    01-JUL-18 ~ 30-JUN-20 H140 : Investigation on Multiblock Scheme for Aerodynamic Analysis of Compressible Flow applied on Complex Geometry to Reduce Computing Time.
    aerodynamic, compressible flow, multiblock scheme, complex geometry, Universiti, RM 20000

    01-SEP-17 ~ 31-AUG-19 U868 : Aircraft Performance Evaluation over a Propeller Driven Aircraft and the Jet Engine Aircraft
    flight performance, fake off, vanding, cruise, Universiti, RM 20000

    01-DEC-15 ~ 30-NOV-17 U416 : Flowfield-Dependent Variation Method For Moving-Boundary Problems
    flowfield dependent variation,moving boudary, finite volume,humerical method, Kebangsaan, RM 20000

    01-MAR-13 ~ 31-AUG-15 1151 : Aerodynamic's Analysis Highly Swept And Delta Wing Through Computational And Experimental By Use Of Particle Image Velocimetry (PIV)
    Aerodynamics,CFD,delta wing, Universiti, RM 37000

    01-MAR-11 ~ 28-FEB-13 0762 : NUMERICAL INVESTIGATION ON THE BEHAVIORS OF VARIOUS EULER SOLVERS IN DEALING WITH SHOCK CAPTURING CAPABILITIES
    , Kebangsaan, RM 51200

    01-MAR-10 ~ 28-FEB-13 0732 : Simulation and Experimental Studies of the Aerodynamics Behaviour of a Small Ducted-Fan Unmanned Aerial Vehicle
    , Kebangsaan, RM 49600

    01-MAR-10 ~ 28-FEB-12 0723 : The Development of Semi Empirical Aerodynamics Formulation for an Aircraft Fuselage Through Wind Tunnel Test
    , Kebangsaan, RM 37600

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