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41
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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42
Separation of palm kernel oil from palm kernel with supercritical carbon dioxide using pressure swing technique
Published 2007“…The pressurization-depressurization treatments are denoted as pressure swing (PS) extractions. Extractions were performed at 353.2 K and at pressures from 10 to 25 MPa. …”
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43
Conus medullary syndrome secondary to spinal cord tumour : report of surgical outcome of 3 cases
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Proceeding Paper -
44
Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
Published 2010“…This research focused on the design, construction and testing of a free wing remote controlled aerial vehicle. The free wing concept allows the wing to move freely in pitch relative to the fuselage. …”
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Proceeding Paper -
45
Effect of angle of incidence on roll damping derivatives of a delta wing
Published 2014“…In the Present paper effect of angle of incidence on roll damping derivative of a delta wing with curved leading edges with attached shock case has been studied. …”
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46
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47
Relationship between pulmonary function and the degree of spinal deformity among adolescent idiopathic scoliosis (AIS) patients
Published 2013“…Kruskal-Wallis and Mann Whitney tests were used to compare the lung function according to different levels of affected spinal vertebrae and the severity of the deformity. …”
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Proceeding Paper -
48
A rare case of monostotic spinal fibrous dysplasia mimicking solitary metastatic lesion of thyroid carcinoma
Published 2016“…Magnetic resonance imaging revealed isolated osteolytic lesion over the posterior element of the T12 vertebra with narrowing of the spinal canal causing compression of the cord. The diagnosis of fibrous dysplasia was made histologically. …”
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Article -
49
Drag analysis of an aircraft wing model and without bird feather like winglet
Published 2012“…This work describes the aerodynamic characteristic for aircraft wing model with and without bird feather like winglet. …”
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Article -
50
Numerical simulation of a low aspect ratio wing at low Reynolds number
Published 2013“…In this work the numerical simulation of aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro aerial vehicle is carried out. …”
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Proceeding Paper -
51
Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
Published 2016“…Aerostatic lift in a hybrid buoyant aircraft reduces the wing loading as well as the induced drag. This reduction is valid till pressure height. …”
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52
Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
Published 2012“…In the present study hypersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with curved leading edges for the attached shock case. …”
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53
Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
Published 2013“…They are applicable for wings of arbitrary plan form shape at high angles of attack provided the shock wave is attached to the leading edge of the wing. …”
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54
The development of a fixed wing aircraft analysis and design flight dynamic software
Published 2016“…Through the implementation of five types of aircraft models, the developed computer code represents a useful tool for flight dynamic analysis and control design for a fixed-wing aircraft.…”
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Thesis -
55
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56
Back pain and osteolysis of the thoracic spine in an adult: a case of monostotic fibrous dysplasia masquerading as spinal metastasis
Published 2013“…MR imaging revealed isolated osteolytic lesion over posterior element of T12 vertebra with narrowing of the spinal canal causing compression to the cord. CT-guided biopsy did not obtain any malignant cells. …”
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Proceeding Paper -
57
Experimental investigation of the vortical flow around a reverse delta wing using PIV
Published 2010“…Particle Image Velocimetry was used in a low speed wind tunnel to investigate the vortex structures of a slender reverse delta wing at various angles of attack and roll. This work investigates the characteristics of the vortices generated downstream in a plane perpendicular to the free stream direction and their dependence on angles of attack and roll angles at chord based Reynolds number.…”
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Proceeding Paper -
58
Prediction of energy absorption capability of curved panel structure; for wing leading edge study
Published 2012“…This paper works on the curvature effect of wing leading edge structure subjected to impact loading. …”
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59
Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
Published 2014“…This paper works on the curvature composite structure for wing leading edge application using fabric carbon/epoxy material subjected to impact loading. …”
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60
Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow
Published 2016“…In this paper attention is focussed on study of effect of Aspect ratio of the wing on roll moment derivatives at various angle of attack and Mach number for a Supersonic flow. …”
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