Inviscid and viscous analysis of three-dimensional turbomachinery flows using an implicit upwind algorithm-Reference-Cited by-同舟云学术

Inviscid and viscous analysis of three-dimensional turbomachinery flows using an implicit upwind algorithm

Published:1996-07-01 Issue: Volume: Page:
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Container-title:32nd Joint Propulsion Conference and Exhibit
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Author:

Benetschik Hannes¹,Lohmann Arnd²,Luecke Juergen²,Gallus Heinz²

Affiliation:

1. Ohio Aerospace Inst.; NASA, Lewis Research Center, Cleveland, OH

2. Inst. fuer Strahlantriebe und Turboarbeitsmaschinen, Aachen, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2556

Reference25 articles.

1. Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. Part I - Methodology

2. W.N. Dawes Unsteady Flow and Loss Production in Centrifugal andAxial Compressor Stages.AGARD-CP571, Jan. 1996.

3. H.Benetschik u.H.E.Gallus.Jnviscid and ViscousTransonic Flows in Cascades Using an Implicit Upwind Algorithm.Journalof Propulsion and Power, Vol. 8, No.2, 1992, pp. 403-409.

4. H. Benetschik. Numerische Berechnung der Trans- und Uberschall-Strdmung in TurbomaschinenmitHilfe eines impliziten Relaxationsverfahrens. Ph.D. Thesis at theRWTH Aachen, FRG, December 1991.

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