Results 111 to 120 of about 142,516 (311)
Dispersal units that continuously rotate while falling purely due to aerodynamic forces are called autorotating dispersal units. Single‐ to multi‐winged forms of autorotating dispersal units occur in nature. The dispersal unit of Getonia floribunda Roxb.
V. V. Drisya +3 more
wiley +1 more source
High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel [PDF]
A wind tunnel investigation of an advanced-technology airfoil was conducted in the Langley 0.3-Meter Transonic Cryogenic Tunnel (TCT). This investigation represents the first in a series of NASA/U.X.
Butler, T. W. +4 more
core +1 more source
ABSTRACT Meeting the rising demand for renewable energy requires innovative solutions to enhance wind power extraction, particularly given demographic and geographic constraints on wind farm deployment. Active high‐lift devices, such as the Active Fluid Gurney Flap (AFGF), offer a promising approach that can dynamically modify aerodynamic performance ...
Mario Lucas, Jorge Saavedra
wiley +1 more source
Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections [PDF]
Theoretical and experimental studies are described which were conducted for the purpose of developing a new generalized method for the prediction of profile drag of single component airfoil sections with sharp trailing edges. This method aims at solution
Goradia, S. H., Lilley, D. E.
core +1 more source
Support Structure Modelling in Actuator Line Method Large Eddy Simulations of Wind Turbine Wakes
ABSTRACT While advancements in the prediction of wind turbine loads and wakes within the actuator line method large eddy simulation (ALM‐LES) framework have been an active research topic in recent years, the modelling of the tower and nacelle has received comparatively less attention.
Markella Zormpa +2 more
wiley +1 more source
This article presents a numerical investigation of the effects of leading-edge protuberances on airfoil stall and post-stall performance. An improved delayed detached eddy simulation (IDDES) method was adopted.
Mingbo Zhao +2 more
semanticscholar +1 more source
Low Reynolds Number Airfoil Evaluation for the Mars Helicopter Rotor
The present research provides a performance comparison between several low Reynolds number airfoil profiles for the Mars Helicopter. The low density of the Martian atmosphere and the relatively small Mars Helicopter rotor result in very low chord-based
Witold J. F. Koning +2 more
semanticscholar +1 more source
This paper focuses on the resilience improvement of the distribution network with high‐penetration new energy under compound temperature–precipitation events (CTPEs). A prediction model of CTPEs‐sources/load based on coupling analysis of meteorological–electrical is proposed to provide data support for subsequent planning research, and a double‐layer ...
Xingyu Luan +5 more
wiley +1 more source
Objectives and approaches to research in turbine heat transfer are discussed. Generally, improvements in the method of determining the hot gas flow through the turbine passage is one area of concern, as is the cooling air flow inside the airfoil, and the
Rohde, J. E.
core +1 more source
Bionic Design of Wind Turbine Blade Based on Long-Eared Owl's Airfoil
The main purpose of this paper is to demonstrate a bionic design for the airfoil of wind turbines inspired by the morphology of Long-eared Owl's wings. Glauert Model was adopted to design the standard blade and the bionic blade, respectively.
W. Tian +6 more
semanticscholar +1 more source

