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Computational Investigation of Wings with Miniature Trailing Edge Control Surfaces
Miniature Trailing Control Surfaces Wing
2015/6/18
Miniature trailing edge e ectors (MiTEs) are small
aps (typically 1% to 5% chord)
actuated with de
ection angles near 90 degrees. The small size, combined with little
required power and good cont...
Computational Investigation of Unsteady Internal Flow in Solid Propellant Rockets
Solid Propellant Rockets Unsteady Compressible Flows
2009/10/14
Unsteady flow in a semi-closed axisymmetric cylindrical channel with steady sidewall mass injection that simulates a model of a solid propellant rocket combustion chamber is studied computationally. P...
Computational investigation of the tensile behaviour of the hard coated Ti-6Al-4V alloy
Computational material science Titanium alloys Surface layer
2010/2/8
Purpose: Modification of the surface layer of the titanium alloys is frequently applied in order to improve their tribological properties. Various surface engineering techniques can be used to produce...