Results 241 to 250 of about 11,271 (298)
This study identifies an immunometabolic axis wherein SAM‐driven PRMT1 methylates LDHA, enhancing its activity. The resultant lactate induces STAT3 K709 lactylation, which stabilizes an active conformation to promote STAT3 phosphorylation and IL‐10 expression.
Hui Wang +12 more
wiley +1 more source
Passive control of wing-tip vortices through a grooved-tip design. [PDF]
Tan J, Ōtomo S, Viola IM, Liu Y.
europepmc +1 more source
Large-gap cascaded Moiré metasurfaces enabling switchable bright-field and phase-contrast imaging compatible with coherent and incoherent light. [PDF]
Li Y +6 more
europepmc +1 more source
Quantum coherent manipulation and readout of superconducting vortex states. [PDF]
Nambisan A +15 more
europepmc +1 more source
Research on the Design of Micromixer Based on Acoustic Streaming-Driven Sharp-Edge Structures. [PDF]
Bai K, Qiao H, Cai J, Hu J, Wang Z.
europepmc +1 more source
Butterfly Clap-Fling Flight Mechanisms Observed by Schlieren Imaging for the Design of Bio-Inspired Micro Air Vehicles. [PDF]
Prisăcariu EG +5 more
europepmc +1 more source
Lift and the Leading Edge Vortex [PDF]
AbstractFlapping wings often feature a leading-edge vortex (LEV) that is thought to enhance the lift generated by the wing. Here the lift on a wing featuring a leading-edge vortex is considered by performing experiments on a translating flat-plate aerofoil that is accelerated from rest in a water towing tank at a fixed angle of attack of 15°.
Pitt Ford, C. W., Babinsky, H.
openaire +3 more sources
Leading edge vortex dynamics [PDF]
Leading edge vortices can create high local pressures which in some situations may be advantageous but in others may cause damage. This paper looks at three wind engineering situations: windborne debris, roof suctions on a low-rise building and pressures near the luff of a downwind sail, where the behaviour of the leading edge vortex is significant. In
Peter J, Richards +1 more
openaire +2 more sources
Dynamic Stall Control by Leading Edge Vortex Generators [PDF]
A new concept of passive dynamic-stall control was developed and tested on an OA209 rotorcraft airfoil during two wind-tunnel test campains in 2004 and 2005. Small vortex generators are mounted at the leading edge of the rotor blade. At low incidence they are located close to the stagnation point and do not impact the flow field.
Mai, Holger +6 more
openaire +4 more sources

