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Oscillating supersonic delta wings with straight leading edges
Published 2012“…A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. …”
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Experimental investigation of plain- and flapped-wing tip vortices
Published 2009“…Particle image velocimetry was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a subsonic wall interference model was used as a vortex generator in two different configurations: 1) plain wing and 2) flapped wing with the trailing-edge flap extended at 20 degrees. …”
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Development of educational software for stress analysis of an aircraft wing
Published 2012“…The developed software can be used to estimate load on a wing and to compute the stresses at any point along the span of the wing of a given aircraft. …”
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Flow visualization over a circular planform wing
Published 2013“…circular plan form wing at high Reynolds numbers has been carried out numerically. …”
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Proceeding Paper -
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Oscillating supersonic delta wings with curved leading edges
Published 2010“…In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. …”
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Evaluation of aircraft wing-tip vortex using PIV
Published 2009“…The formation and development of a wing-tip vortex in a near and extended near filed were studied experimentally. …”
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Proceeding Paper -
27
iKool ointment - 10% eucalyptus oil, 5% peppermint oil, 5% menthol, 5% camphor
Published 2020“…Label displaying the brand name iKool and main ingredients i.e 10% eucalyptus oil, 5% peppermint oil, 5% menthol, 5% camphor in ointment bases, with other instruction and labeling as required by regulatory.…”
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Back pain and osteolysis of the thoracic spine in an adult: a case of monostotic fibrous dysplasia masquerading as spinal metastasis
Published 2013“…The diagnosis of fibrous dysplasia was made histologically. Five months post-surgery, the patient’s condition improved gradually. …”
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Proceeding Paper -
29
Book Review, Military Legal Proceedings in Malaysia: Teo Say Eng & Colonel Wan Nor Mazlan (2009), LexisNexis(HardCover)
Published 2010“…It provides guide for those directly involved in courts-martial proceedings such as the defence counsel and the courts' officers, including the judges of the courts-martial. 4 However, it was suggested in the book review that few matters regarding substance and technical parts of the book should be improved to make it more informative and useful. 5…”
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Untitled (Group of five men)
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Group portrait of five men
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Firearm recognition based on whole firing pin impression image via backpropagation neural network
Published 2011“…In this study, a set of data which focused on selected 6 features of firing pin impression images before an entirety of five different pistols of South African made; the Parabellum Vector SPI 9mm model, were used. …”
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Book Chapter -
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Firearm recognition based on whole firing pin impression image via backpropagation neural network
Published 2011“…In this study, a set of data which focused on selected 6 features of firing pin impression images before an entirety of five different pistols of South African made; the Parabellum Vector SPI 9mm model, were used. …”
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Proceeding Paper -
35
Bayatyan v Armenia
Published 2012“…This article discusses the recent landmark judgment in the case of Bayatyan v Armenia (No. 23459/03) 7.07.11 in which the European Court of Human Rights (ECtHR) broke with previous case law and decided to include conscientious objectors within the scope of Art. 9 of the European Convention on Human Rights (ECHR): the right to freedom of thought, conscience and religion.…”
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Frequency reconfiguration mechanism of a PIN diode on a reconfigurable antenna for LTE and WLAN Applications
Published 2018“…In this work, a frequency reconfigurable antenna with a BAR63-02V Positive-Intrinsic-Negative (PIN) diode is designed, simulated and fabricated. …”
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Induced rolling moment for NACA4412 plain and flapped wing
Published 2010“…Purpose – The paper aims to compute rolling moments on a follower aircraft wing due to vortices generated by a plain and flapped NACA4412 wing using experimental particle image velocimetery (PIV) data. …”
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Investigation of the vortical flow around a reverse delta wing
Published 2011“…A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta wing.…”
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Proceeding Paper -
40
Estimation of stability derivatives of a delta wing in hypersonic flow
Published 2012“…In the present study supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for attached shock case. A strip theory is used in which strips at different span wise locations are independent. …”
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Article