Development of an explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachinery-Reference-Cited by-同舟云学术

Development of an explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachinery

Published:1986-01-06 Issue: Volume: Page:
ISSN:
Container-title:24th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

CHIMA R.¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-32

Reference25 articles.

1. Solution of Plane Cascade Flow Using Improved Surface Singularity Methods

2. Second-Order-Accurate Calculation of Transonic Flow over Turbomachinery Cascades

3. Application of Runge Kutta time marching scheme for the computation of transonic flows in turbomachines

4. Steger, J.L., Pulliam, T.H., and Chima, R.V. "An Implicit Finite-Difference Code for Inviscid and Viscous Cascade Flow,''AIAA Paper 80-1427, July 198C.

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2. An unstructured adaptive quadrilateral mesh-based scheme for viscousturbomachinery flow calculations;29th Joint Propulsion Conference and Exhibit;1993-06-28

3. Quasi-3D viscous flow computations in subsonic and transonic turbomachinery bladings;26th Joint Propulsion Conference;1990-07-16

4. Computational Analysis of Rotor-Stator Interaction in Turbomachinery Using Zonal Techniques;Applied Computational Aerodynamics;1990-01-01

5. Three-dimensional multigrid Navier-Stokes computations for turbomachinery applications;25th Joint Propulsion Conference;1989-07-12