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0026898307
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Design method for subsonic and transonic cascades with prescribed mach number distribution
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Leonard, O., and Van den Braembussche, R. A., 1992, "Design Method for Subsonic and Transonic Cascades with Prescribed Mach Number Distribution," ASME J. Turbomach., 114(3), pp. 553-560.
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Three-dimensional inverse method for turbomachinery blading design
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A two-dimensional Navier-Stokes inverse solver for compressor and turbine blade design
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An inverse method for the design of transonic airfoils and wings
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A Navier-Stokes solver for turbomachinery applications
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Arnone, A.1
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8
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On upstream differencing and Godunov-type schemes for hyperbolic conservation laws
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Restoration of the contact surface in the HLL-Riemann solver
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13
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von Karman Institute, TN 174
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Arts, T., Lambert de Rouvroit, M., and Rutherford, A. W., 1990, "Aero-Thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade," von Karman Institute, TN 174.
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Aero-Thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade
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Arts, T.1
Lambert de Rouvroit, M.2
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