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Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Investigations of flutter in transonic turbine cascades have shown that the movement of unsteady normal shocks has an important effect on the excitation of blades. In order to predict this ...
Erratum: “Numerical Simulation of Inviscid Transonic Flow Through Nozzles With Fluctuating Back Pressure” (Journal of Turbomachinery, 1989, 111, pp. 169–180)
Publisher: The American Society of Mechanical Engineers (ASME)
Numerical Simulation of Inviscid Transonic Flow Through Nozzles With Fluctuating Back Pressure
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The study presents a numerical method, based on the flux vector splitting approach, to the problem of unsteady one-dimensional and two-dimensional inviscid transonic flows, with emphasis on the ...
Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi-Three-Dimensional Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents a new International Standard Configuration to be added to an already existing set of 10 configurations for unsteady flow through vibrating axial-flow turbomachine cascades. ...
An International Electronic and Interactive Teaching and Life-Long Learning Platform for Gas Turbine Technology in the 21st Century
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An interactive learning platform which sets a new standard for electronic learning of gas turbine technology in a global life-long learning perspective is presented (Fig. 1). The platform contains ...