Results 211 to 220 of about 788,444 (280)

Adaptation of Echinococcus Multilocularis to Oxidative Stress Depends on EmPDK‐Mediated Metabolic Reprogramming

open access: yesAdvanced Science, EarlyView.
Metabolic adaption presents a vital survival strategy for E. multilocularis. This study identifies EmPDK as a central metabolic regulator governing glucose metabolic reprogramming. Oxidative stress activates EmHIF1α to induce EmPDK expression. Mechanistic characterization reveals this ROS/EmHIF1α/EmPDK axis drives glycolytic reprogramming to sustain ...
Huijuan Wang   +5 more
wiley   +1 more source

Extracorporeal Support Vascular Access: 3D Printing Custom Cannulas. [PDF]

open access: yesASAIO J
Zhang A   +11 more
europepmc   +1 more source

Regional venous-to-arterial carbon dioxide pressure and content differences during endotoxemic shock: influence of hydrogen ion accumulation vs. Haldane effect. [PDF]

open access: yesIntensive Care Med Exp
Ospina-Tascón GA   +8 more
europepmc   +1 more source

Steady and unsteady transonic flow

16th Aerospace Sciences Meeting, 1978
An investigation of the transonic flow over a circular arc airfoil was conducted to obtain basic information for turbulence modeling of shock-induced separated flows and to verify numerical computer codes which are being developed to simulate such flows. The investigation included the employment of a laser velocimeter to obtain data concerning the mean
H. L. Seegmiller   +2 more
openaire   +1 more source

Transonic flow in unconventional nozzles.

AIAA Journal, 1968
The description of the compressible gas flow in the throat region of unconventional rocket nozzles must be known in order to optimize the wall contours and to predict the performance. The existence of both subsonic and supersonic flow in close proximity does not permit the use of conventional analytical techniques to obtain a mathematical description ...
Hopkins, D. F., Hill, D. E.
openaire   +2 more sources

The Stabilization Law for Transonic Flow

SIAM Journal on Applied Mathematics, 1986
The stabilization law for transonic flow expresses the experimentally observed freezing of the local Mach number near the airfoil and ahead of the shock at free stream Mach numbers near one. Mathematically this means that near Mach one the flow over an airfoil is a small perturbation of sonic flow.
Cook, L. Pamela, Zeigler, F. J.
openaire   +1 more source

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