Abstract The aim of this study is to investigate the fluid flow structure and heat transfer from an isothermal cylinder with a curved corner radius ratio ( r/R ) 0.5, attack angle α varied between 0° ≤ 45°. subjected airflow at Reynolds number Re = 180 Prandtl Pr 0.7. This focuses on effect forces, Strouhal number, Nusselt structure, wake bubble size. sensitivity time-mean drag lift forces inve...

AIM Using the newly developed scanning peripheral anterior chamber depth analyser (SPAC), the effects of peripheral laser iridotomy (PLI) on peripheral anterior chamber depth (PACD) were determined quantitatively as was the association between PACD and chronic elevation of intraocular pressure (IOP) after PLI. METHODS 16 eyes of 15 patients with acute primary angle closure glaucoma (PACG) att...

T he crystalline lens has a pivotal role in primary angle closure (PAC), both in the pathogenesis of pupil block and by exacerbating the effect of non-pupil block mechanisms such as peripheral iris crowding. Eyes with angle closure tend to have shallow anterior chambers and thick, anteriorly positioned lenses when compared with normal eyes. Removing the lens creates more space in the anterior c...

noses by using the equivalent axisymmetric body (EAB) theory. This Code has been developed by researchers and the results of it have been validated by the various flight tests results. In the case of non-zero angle of attack or asymmetric surface ablation for each meriodinal plane, the equivalent meriodinal plane (EMP) is created for any meriodinal plane. The combinations of these planes consti...

In this work, we discuss physical layer message manipulation attacks, in which an attacker changes physical-layer properties of an original wireless message. Instead of targeting the data content of the message, those attacks target message properties such as time-of-arrival, signal strength, angle-of-arrival, and others. As such attacks do not change the data content, they do not violate the m...

determining characteristics and behavior of fluid flow and obtaining the aerodynamic coefficients are important and considerable tasks in investigation of flow over the bodies. in this research, leading edge radius effects on the flow behavior over a delta wing with a sweep angle of 50 degree at different reynolds numbers between 0.5×106 and 2.5×106 are investigated numerically. three different...