Results 61 to 70 of about 179,245 (211)
, 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
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Archives 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
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Maximum two-phase flow rates of subcooled nitrogen through a sharp-edged orifice [PDF]
Data are presented of an experiment in which subcooled liquid nitrogen was discharged through a sharp-edged orifice at flow rates near the maximum.
Simoneau, R. J.
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Experimental stagnation point velocity gradients and heat transfer coefficients for a family of blunt bodies at Mach 8 and angles of attack [PDF]
Stagnation pressure and heat transfer measurements of blunt axisymmetric ...
Ellison, J. C.
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A new flow model for highly separated airfoil flows at low speeds [PDF]
An analytical model for separated airfoil flows is presented which is based on experimentally observed physical phenomena. These include a free stagnation point aft of the airfoil and a standing vortex in the separated region.
Naik, S. N., Zumwalt, G. W.
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, 2013 The structure of a hydrodynamic, double transonic flow driven by neutrino annihilation in the polar region of a Schwarzschild black hole is computed for different energy deposition profiles.
Globus, Noemie, Levinson, Amir
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Extensional rheology and elastic instabilities of a wormlike micellar solution in a microfluidic cross-slot device [PDF]
, 2012 Wormlike micellar surfactant solutions are encountered in a wide variety of important applications, including enhanced oil recovery and ink-jet printing, in which the fluids are subjected to high extensional strain rates.
Alves, M.A. +4 more
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Pressure distributions from high Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel [PDF]
Tests were conducted in the 2-D test section of the Langley 0.3-meter Transonic Cryogenic Tunnel on a NACA 0012 airfoil to obtain aerodynamic data as a part of the Advanced Technology Airfoil Test (ATAT) program.
Hill, Acquilla S. +2 more
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Cross-talk between topological defects in different fields revealed by nematic microfluidics [PDF]
, 2017 Topological defects are singularities in material fields that play a vital role across a range of systems: from cosmic microwave background polarization to superconductors, and biological materials.
Giomi, Luca +3 more
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Journal of Applied Fluid Mechanics, 2016 Numerical simulations have been carried out to examine the performance and flow parameters of forced rotating vaneless diffuser obtained by the extension of impeller disks of a low-pressure ratio shrouded type centrifugal compressor stage with diffuser ...
S. Seralathan, D. G. Roy Chowdhury
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