Mujahid Samad SuhaebJakarta Aerospace [JAe], Indonesia · Corporate
Mujahid Samad Suhaeb
Doctorate
About
2
Publications
294
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21
Citations
Introduction
An Experimental Investigation and Computational Fluid Dynamics [CFD] Assessment for the Aerodynamics of Battle Damage Finite Aspect Ratio Wing.
The purpose was to determine how span-wise location of single hole simulating gunfire damage influences the aerodynamic characteristics of a finite aspect ratio wing
Additional affiliations
December 2001 - December 2005
Publications
Publications (2)
Numerical studies have been carried out on a battle damaged NACA 641-412 half wing of aspect ratio 8.2 at a Reynolds number of 5.5 x 105. The simulated gunfire damage was represented by a single hole with a diameter of 0.2 wing chord. The hole was centred at half chord and at spanwise locations of 450mm and 650mm from wing root. Computational Fluid...
This article is closed access. It was published in the Journal of Aircraft [© American Institute of Aeronautics and Astronautics] and is available from: http://dx.doi.org/10.2514/1.39839 Wind-tunnel tests have been carried out on a battle-damaged NACA 641–412 half-wing aspect ratio of 8.2. The simulated gunfire damage had a diameter of 0.2 wing cho...
