Results 291 to 300 of about 47,947 (362)

Numerical Investigation of Aerodynamic Uncertainties Caused by Turbulence Modeling for a Missile in Transonic Flow

Salih Kagan Durmus, Nilay Sezer Uzol
openalex   +2 more sources

Quantifying the effect of IMPEDE-FX packing rate and volume on pressure-normalized principal wall strain in an idealized 3D-printed aneurysm model. [PDF]

JVS Vasc Sci
Kedwai B, Geiger J, Najjar S, Kruger J, Richards M, Yeh C, Dennehy M, Stoner M, Mix D.   +8 more
europepmc   +1 more source

Hemodialysis Access Blood Flow and Cardiopulmonary Outcomes. [PDF]

Cureus
Mondal Z, Jalalzadeh M, Khalil S.
europepmc   +1 more source

Evaluating the role of graft angle on cerebral hemodynamics following direct cerebral bypass for moyamoya disease. [PDF]

PLoS One
Peng C, Church EW, Brindise MC.
europepmc   +1 more source

Experimental Estimation of Kinematic Viscosity of Low-Density Air Using Optically Derived Macroscopic Transient Flow Parameters. [PDF]

Sensors (Basel)
Miś TA.
europepmc   +1 more source

Hyperoxia does not improve the acute upper thermal tolerance of a tropical marine fish (Lutjanus apodus).

J Exp Biol
Sandrelli RM, Porter ES, Gamperl AK.
europepmc   +1 more source

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Transonic swirling flow.

AIAA Journal, 1969
An approximation that can be used to determine how swirl affects the choking constraint on flow through the throat of a nozzle is obtained. The flow model is consistent with an experimentally observed flow pattern that contains a recirculating internal cell upstream of the throat.
W. S. LEWELLEN, W. J. BURNS, H. J. STRICKLAND   +2 more
openaire   +1 more source

Flow in Transonic Compressors

AIAA Journal, 1980
Introduction B the term transonic compressor we mean an axial flow compressor in which the inlet flow Mach number, relative to the rotating blades, varies from below unity at radii near the inner casing or hub to values substantially above unity at radii near the blade tips.
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MIXED EQUATIONS AND TRANSONIC FLOW

Journal of Hyperbolic Differential Equations, 2004
This paper reviews the present situation with existence and uniqueness theorems for mixed equations and their application to the problems of transonic flow. Some new problems are introduced and discussed. After a very brief discussion of time-dependent flows (Sec. 1) the steady state and its history is described in Sec. 2. In Secs.
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TRANSONIC OBLIQUE-WING FLOW COMPUTATION

The Quarterly Journal of Mechanics and Applied Mathematics, 1984
Starting from a survey about some modern methods of numerical computations of transonic flow fields an asymptotic method of calculating the steady transonic flow about a large-aspect-ratio wing with inclination or sweep to the direction of motion is derived which is in connection with the well known lifting-line theory.
Evans, T., Cheng, H. K.
openaire   +1 more source