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Chest compression superimposed with sustained inflation - translating preclinical findings into a neonatal clinical trial. [PDF]
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Investigation of pressure gain characteristics for kerosene-hot air RDE
Combustion and Flame, 2023Xingkui Yang, Jianping Zhou, Shida Xu
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The evolution of pressure gain in turbulent fast flames
Combustion and Flame, 2021Abstract This research quantifies the evolution of pressure for fast burning regimes characterized by various degrees of compressibility and involving turbulent flames and shocks. The experimental exploration is conducted in a Turbulent Shock Tube facility, where the level of flame compressibility is controlled by varying the equivalence ratio of the
Hardeo M. Chin +5 more
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Gain spectrum of a high‐pressure CO2laser
Applied Physics Letters, 1975The gain spectrum of a high-pressure uv preionized CO2 laser was measured for pressures to 14 atm. The data show an ∼10% increase in the gain of the P branch of the 961-cm−1 (00°1) - (10°0)1 band which is attributed to the overlapping 927-cm−1 0111- (1110)1 band.
J. L. Miller +2 more
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Autoignition in stratified mixtures for pressure gain combustion
Proceedings of the Combustion Institute, 2021The reliable generation of quasi-homogeneous autoignition inside a combustor fed by a continuous air flow would represent a milestone in realizing pressure gain combustion in gas turbines. In this work, the ignition distribution inside a stratified fuel–air mixture is analyzed. The ability of precise and reproducible injection of a desired fuel profile
Fatma Cansu Yücel +3 more
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Theoretical analysis on the total pressure gain of rotating detonation systems
Combustion and Flame, 2023Wenqi Fan, Haocheng Wen
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Evaluation of Uncertainties of Pressure Gain Measurements in Rotating Detonation Combustor
AIAA Journal, 2023Experimentally measuring the pressure gain of a rotating detonation combustor through the method of equivalent available pressure is prone to many experimental uncertainties.
A. Feleo, Mirko Gamba
semanticscholar +1 more source
Journal of Fluids Engineering, 2022
The blade leading edge is a design variable that can affect the local flow patterns and pressure peaks, which imply a direct effect on the cavitation performance.
Yong-In Kim +3 more
semanticscholar +1 more source
The blade leading edge is a design variable that can affect the local flow patterns and pressure peaks, which imply a direct effect on the cavitation performance.
Yong-In Kim +3 more
semanticscholar +1 more source