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Advanced blade profiles for improved efficiency in Savonius wind turbines: the aeroleaf case study. [PDF]
Sci RepHosseinian SM, Mohseni M, Karimi MS.
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Haemodynamic Performance of Transcatheter Heart Valve in Bileaflet Mechanical Valve: An In-vitro Study. [PDF]
Interdiscip Cardiovasc Thorac SurgCatalano C +5 more
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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 +2 more
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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 +2 more
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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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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, 2004This 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, 1984Starting 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.
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