Effect-size-based electrode and feature selection for emotion recognition from EEG
(2013)
Presentation / Conference Contribution
Outputs (114)
Scavenge flow in a bearing chamber with tangential sump off-take (2013)
Journal Article
A tangential sump design is employed in several aero-engines mainly due to its simplicity and compactness. However various problems have prompted investigations of the sump design. An experimental program at Purdue University (Chandra, 2006, "Flows i... Read More about Scavenge flow in a bearing chamber with tangential sump off-take.
Study of gas/liquid behavior within an aeroengine bearing chamber (2013)
Journal Article
Aeroengine bearing chambers typically contain bearings, seals, shafts and static parts. Oil is introduced for lubrication and cooling and this creates a two phase flow environment that may contain droplets, mist, film, ligaments, froth or foam and li... Read More about Study of gas/liquid behavior within an aeroengine bearing chamber.
Haptic perception of material properties and implications for applications (2013)
Journal Article
Perceiving the material properties of objects through touch is generally superior to the perception of shape. We review major material properties accessible through haptic interaction, along with theoretical accounts of the underlying perceptual proc... Read More about Haptic perception of material properties and implications for applications.
Inverse kinematics for shape rendering interfaces (2013)
Presentation / Conference Contribution
Determining the reliable minimum unit capacitance for the DAC capacitor array of SAR ADCs (2013)
Journal Article
The layout area of an SAR ADC is mainly occupied by its DAC capacitor array. Since there are 2 matched unit capacitors employed for a binary-weighted N-bit DAC, selecting a small unit capacitance is the key to reducing the layout area of the capacit... Read More about Determining the reliable minimum unit capacitance for the DAC capacitor array of SAR ADCs.
An engineering method using a 2D unsteady potential formulation (called the free vortex model or FVM) has been developed to predict the normal force, centre-of-pressure and vortex position for cruciform wing-body combinations in the “plus” orientatio... Read More about An engineering method for modeling the interaction of circular bodies and very low aspect ratio cruciform wings at supersonic speeds.
Scramjet flow and intake SBLI: Technical challenges and case study (2013)
Journal Article
This paper reviews some basic research areas associated with Scramjet-powered hypersonic flying vehicle, particularly the forebody boundary-layer transition and intake shock-wave boundary-layer interactions (SBLI). Some technical and physical challen... Read More about Scramjet flow and intake SBLI: Technical challenges and case study.
Effect of mesh topologies on wall heat transfer and pressure loss prediction of a blade coolant passage (2013)
Presentation / Conference Contribution
This paper studies the effect of mesh topologies such as hybrid and structured meshes on the evaluation of wall heat transfer coefficient (HTC) and pressure loss of a blade cooling passage. An experimental model is chosen; it has five-row of stream w... Read More about Effect of mesh topologies on wall heat transfer and pressure loss prediction of a blade coolant passage.
A review of the manufacture, mechanical properties and potential applications of auxetic foams (2013)
Journal Article
Auxetics are a modern class of material fabricated by altering the material microstructure. Unlike conventional materials, auxetics exhibit a negative Poisson's ratio when subjected to tensile loading. These materials have gained popularity within th... Read More about A review of the manufacture, mechanical properties and potential applications of auxetic foams.