Results 21 to 30 of about 7,951,401 (343)
Experimental Investigation on the Combined Blowing Control of a Hybrid Wing Body Aircraft
Actuators, 2023 Combined blowing was performed on a Hybrid Wing Body (HWB) aircraft through wind tunnel testing at a Reynolds number of 1.75 × 106. The full cycle of separation and reattachment under the control of combined blowing was implemented using Computational ...
Jiaxin Pan +5 more
doaj +1 more source
Drag and lift forces on a counter-rotating cylinder in rotating flow [PDF]
, 2010 Results are reported of an experimental investigation into the motion of a heavy cylinder free to move inside a water-filled drum rotating around a horizontal axis.
CHAO SUN +8 more
core +8 more sources
Evolution of the leading-edge vortex over a flapping wing mechanism
Journal of Mechanical Engineering and Sciences, 2020 Leading-edge vortex governs the aerodynamic force production of flapping wing flyers. The primary factor for lift enhancement is the leading-edge vortex (LEV) that allows for stall delay that is associated with unsteady fluid flow and thus generating ...
Muhamad Ridzuan Arifin +6 more
doaj +1 more source
Effect of Multistage Circulation Control on Blade Aerodynamic Performance
Energies, 2022 To improve the low aerodynamic efficiency and reduce the high energy consumption of a single-stage circulation control wing, a multistage circulation control wing was designed.
Hai Du +4 more
doaj +1 more source
Coriolis effects enhance lift on revolving wings [PDF]
Physical Review E, 2015 At high angles of attack, an aircraft wing stalls. This dreaded event is characterized by the development of a leading edge vortex on the upper surface of the wing, followed by its shedding which causes a drastic drop in the aerodynamic lift. At similar angles of attack, the leading edge vortex on an insect wing or an autorotating seed membrane remains
Jardin, Thierry, David, Laurent
openaire +4 more sources
Application Research of Flow Control Using Co-flow Jet on a Vertical Tail
Hangkong gongcheng jinzhan, 2022 The aerodynamic characteristics of the vertical tail of an aircraft are directly related to the size and weight of the vertical tail. Increasing the lift force of the vertical tail using flow control can further reduce the size of the vertical tail,which
SHI Zijie +5 more
doaj +1 more source
Indian Journal of Ophthalmology, 2023 Purpose: To compare visual outcomes of early enhancement following small incision lenticule extraction (SMILE) versus laser in situ keratomileusis (LASIK). Methods: Retrospective analysis of eyes (patients operated in the setting of a tertiary eye care
B Soundarya +4 more
doaj +1 more source
Review of the Co-flow Jet Flow Control Method
Hangkong gongcheng jinzhan, 2022 The co-flow jet(CFJ)is a new concept flow control method based on blowing and suction technology.Since it was proposed,it has gradually attracted extensive attention.This paper reviews the basic principles,concepts,research methods and progress of CFJ ...
XU Heyong, MA Chengyu
doaj +1 more source
Lift Enhancement for Low-Aspect-Ratio Wings with Periodic Excitation [PDF]
, 2010 In an effort to enhance lift on low-aspect-ratio rectangular flat-plate wings in low-Reynolds-number post-stall flows, periodic injection of momentum is considered along the trailing edge in this numerical study.
Colonius, Tim +3 more
core +1 more source
Aerodynamic Exploration for Tandem Wings with Smooth or Corrugated Surfaces at Low Reynolds Number
Aerospace, 2023 Skin corrugation and tandem configuration are two distinct features that characterize the flow around dragonfly wings. In contrast to the smooth airfoil and single pair of wings of conventional airplanes, corrugated surfaces and tandem wings influence ...
Qing Zhang, Rongrong Xue, Heng Li
doaj +1 more source