Results 71 to 80 of about 159,512 (193)

Mounting pressure on Russia's government budget

open access: yes, 2019
SWP Research Paper 2 ...
Kluge, Janis   +1 more
openaire   +3 more sources

Pressure distribution in a converging-diverging nozzle during two-phase choked flow of subcooled nitrogen [PDF]

open access: yes
Choked flow rates and axial pressure distributions were measured for subcooled nitrogen in a converging-diverging nozzle with a constant area section in the throat region.
Simoneau, R. J.
core   +1 more source

Flow Field in the Turbine Rotor Passage in an Automotive Torque Converter Based on the High Frequency Response Rotating Five-hole Probe Measurement Part I: Flow Field at the Design Condition (Speed Ratio 0.6)

open access: yesInternational Journal of Rotating Machinery, 2001
The relative flow field in an automotive torque converter turbine was measured at three locations inside the passage (turbine 1/4 chord, mid-chord, and 4/4 chord) using a highfrequency response rotating five-hole-probe.
Y. F. Liu   +2 more
doaj   +1 more source

On the Hydrodynamic Interplay Between a Young Nuclear Starburst and a Central Super Massive Black Hole

open access: yes, 2010
We present 1D numerical simulations, which consider the effects of radiative cooling and gravity on the hydrodynamics of the matter reinserted by stellar winds and supernovae within young nuclear starbursts with a central supermassive black hole (SMBH ...
Alexander   +33 more
core   +1 more source

Two-phase choked flow of subcooled nitrogen through a slit [PDF]

open access: yes
Two-phase choked flow rate and pressure distribution data are reported for subcooled nitrogen flowing through a slit. The slip was a narrow rectangular passage of equal length and width. The inlet stagnation pressure ranged from slightly above saturation
Simoneau, R. J.
core   +1 more source

On the influence of the nozzle external configuration on the radiated screech and the decay of supersonic jets

open access: yesArchives of Acoustics, 2016
The behaviour of screeching jets exhausting from an axisymmetric con-vergent-divergent nozzle was studied. The nozzle had a 2.9 mm throat diameter and a. 1.95 theoretical exit Mach number.
Giovanni Maria CARLOMAGNO   +2 more
doaj  

MHD oblique stagnation-point flow of a Newtonian fluid [PDF]

open access: yes, 2011
The steady two-dimensional oblique stagnation-point flow of an electrically conducting Newtonian fluid in the presence of a uniform external electromagnetic field (E0, H0) is analyzed, and some physical situations are examined.
Borrelli, Alessandra   +2 more
core   +1 more source

Micrometer-sized droplets from liquid helium jets at low stagnation pressures [PDF]

open access: hybrid, 2022
Katharina Kolatzki   +5 more
openalex   +1 more source

Aerothermodynamic Analysis of a Reentry Brazilian Satellite

open access: yes, 2012
This work deals with a computational investigation on the small ballistic reentry Brazilian vehicle SARA (acronyms for SAt\'elite de Reentrada Atmosf\'erica). Hypersonic flows over the vehicle SARA at zero-degree angle of attack in a chemical equilibrium
AL Garcia   +24 more
core   +1 more source

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