Results 1 to 10 of about 47,693 (267)
Background This study aimed to assess initial results and patient characteristics of prostatic urethral lift (PUL) compared with those of bipolar transurethral enucleation of the prostate (TUEB) in the treatment of benign prostatic hyperplasia (BPH) in ...
Daisuke Obinata +7 more
doaj +3 more sources
Induced (E,M)−structures on Topological Categories
In this paper, we describe a convenient categorical structure with respect to a class of monomorphisms M and epimorphisms E for any topological category.
Juan Angoa Amador +2 more
doaj +1 more source
Single-Objective Optimal Design of a High-Performance Wind Turbine Airfoil Family
The development of high-performance wind turbine blade airfoil families is an important research topic in wind power generation technology. Using the NACA63 series airfoil as the initial airfoil, the XFOIL software based on the panel method is used to ...
Zhaohuang Zhang +3 more
doaj +1 more source
Aerodynamic Shape Optimization of a NACA0018 Airfoil Using Adjoint Method and Gradient-Based Optimizer [PDF]
The purpose of this study is to demonstrate the suitability and efficacy of the adjoint method on the aerodynamic shape optimization on a simple symmetrical airfoil NACA0018 at low Reynolds number for wind turbine application. The adjoint method has been
van Stratan G.S.M. +2 more
doaj +1 more source
Vertical Launch Trajectory Modeling and Range Influence Law of Shipborne Depth Charge
The vertical launch of shipborne depth charge can greatly improve platform adaptability and combat effectiveness, which is of great significance in improving the combat capability of ships.
Xiaohui WAN +5 more
doaj +1 more source
In this study, the aerodynamic performance characteristics of three new EYO-Series low Reynolds number (Re) airfoils were tested at Re = 100,000 to 500,000, which are typical range of Re numbers encountered by airfoils of small wind turbine blades.
Emmanuel Yeboah Osei +4 more
doaj +1 more source
Aerodynamic Analysis of Retractable Belly Flap for a Flying Wing Aircraft
The study on the lift enhancement effect of the retractable belly flap on the flying wing configuration can conclude the effect rules on aircraft aerodynamic force.
CHEN Xian +4 more
doaj +1 more source
Sectional Leading Edge Vortex Lift and Drag Coefficients of Autorotating Samaras
Autorotating samaras such as Sycamore seeds are capable of descending at exceptionally slow speeds and the secret behind this characteristic is attributed to a flow mechanism known as the leading edge vortex (LEV).
Byung Kwon Jung, Djamel Rezgui
doaj +1 more source
In this paper, a pitching airfoil near flat and wavy ground is studied by numerical simulations. The kinematic features of the airfoil and the flow field around it are analyzed to reveal unsteady vorticity dynamics of the self-propelled airfoil in ground
Zhiqiang Xin +3 more
doaj +1 more source
Object size effects on initial lifting forces under microgravity conditions [PDF]
Individuals usually report for two objects of equal mass but different volume that the larger object feels lighter. This so-called size-weight illusion has been investigated for more than a century. The illusion is accompanied by increased forces, used to lift the larger object, resulting in a higher initial lifting speed and acceleration. The illusion
Kingma, I. +2 more
openaire +3 more sources

