Results 11 to 20 of about 7,951,401 (343)

Covas-Lift: Facial Enhancement [PDF]

open access: yesotolaryngology, 2017
Objective: 1) Describe our results as a new surgical option in facial enhancement. 2) Establish the indications and steps in the procedure. 3) Show before and after results. Method: From March 2010 until October 2016 we analyzed 647 successive cases performed in our surgical department.
Jose L Covarrubias   +3 more
openaire   +2 more sources

Experimental Investigation of Lift Enhancement and Drag Reduction of Rotor Airfoil Using Co-flow Jet Concept

open access: yesHangkong gongcheng jinzhan, 2021
As the novel active flow control technology,Co-flow Jet concept(CFJ)is one of the most potential methods to achieve the high lift enhancement and drag reduction of rotor airfoil.Based on the OA 312 rotor airfoil,the CFJ rotor airfoil dynamometric model ...
ZHANG Shunlei   +4 more
doaj   +1 more source

A Boundary-Vorticity Perspective on Lift Enhancement at Ultra-Low Reynolds Numbers

open access: yesJournal of Aerospace Sciences and Technologies, 2023
The ultra-low Reynolds number flow over airfoils is considered from the perspective of boundary vorticity dynamics in this paper. The dynamic balance between the streamwise pressure gradient and vorticity creation rate at the wall is highlighted by the ...
N. Rashmi, M. Sivapragasam
semanticscholar   +1 more source

Lift Enhancement on Oscillating Airfoils [PDF]

open access: yes39th AIAA Fluid Dynamics Conference, 2009
Force and particle image velocimetry measurements were conducted on a NACA 0012 airfoil undergoing sinusoidal plunge oscillations at amplitudes of 2.5% to 20% of chord, a post-stall angle of attack of 15°, and Reynolds number of 10,000. It was shown that airfoil oscillations significantly increase lift and reduce drag. Lift improvement is primarily due
Cleaver, David   +2 more
openaire   +1 more source

Effects of Plasma Actuator Discharge on Lift-Enhancement and Flow Patterns of Flying Wing Aircraft [PDF]

open access: yesXibei Gongye Daxue Xuebao, 2018
The nanosecond pulsed plasma discharge actuator is used on a flying wing aircraft. At the angles of attack rang from -4° to 28°, the impact of plasma actuator arrangement position and discharge frequency on lift-enhancement effect is tested.

doaj   +1 more source

Facial Rejuvenation Enhancing Cheek Lift [PDF]

open access: yesArchives of Plastic Surgery, 2017
Supported by recent literature on the signs of aging of the middle and lower face, our clinical research has documented a loss of volume of the deep structural components of the central face and a progressive descent of the nasolabial fat and the jowl fat, leading to facial fragmentation.
Philippe Bellity, Jonathan Bellity
openaire   +3 more sources

Aerodynamic Analysis of Retractable Belly Flap for a Flying Wing Aircraft

open access: yesHangkong gongcheng jinzhan, 2022
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

Mechanism of Magnetic Flux Leakage Detection Method Based on the Slotted Ferromagnetic Lift-Off Layer

open access: yesSensors, 2022
Magnetic flux leakage (MFL) testing is widely used in non-destructive testing of ferromagnetic components. In view of the serious attenuation of the leakage magnetic field (LMF) caused by the transmission of LMF in the lift-off layer between the ...
Jian Tang   +4 more
doaj   +1 more source

Lift observation conveys object weight distribution but partly enhances predictive lift planning [PDF]

open access: yesJournal of Neurophysiology, 2020
AbstractObservation of object lifting allows updating of internal object representations for object weight, in turn enabling accurate scaling of fingertip forces when lifting the same object. Here, we investigated whether lift observation also enables updating of internal representations for an object’s weight distribution.
Guy Rens   +3 more
openaire   +4 more sources

Clap-and-Fling Mechanism in Non-Zero Inflow of a Tailless Two-Winged Flapping-Wing Micro Air Vehicle

open access: yesAerospace, 2022
The aerodynamic performance of clap-and-fling mechanism in a KU-Beetle—a tailless two-winged flapping-wing micro air vehicle—was investigated for various horizontal free-stream inflows.
Loan Thi Kim Au   +3 more
doaj   +1 more source

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