Solution-adaptive structured-unstructured grid method for unsteady turbomachinery analysis. I - Methodology

Author:

Mathur Sanjay R.1,Madavan Nateri K.2,Rajagopalan R. Ganesh1

Affiliation:

1. Iowa State University, Ames, Iowa 50011

2. MCAT Institute, NASA Ames Research Center, Moffett Field, California 94035

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Hybrid mesh smoothing based on Riemannian metric non-conformity minimization;Finite Elements in Analysis and Design;2010-01

2. Flow Simulation Using Generalized Static and Dynamic Grids;AIAA Journal;1999-12

3. The development of an Euler/Navier-Stokes flow solver for all speeds on 2D unstructured meshes;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

4. Navier-Stokes flow simulation on hybrid grids;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

5. Mesh Smoothing Based on Riemannian Metric Non-Conformity Minimization;Proceedings of the 15th International Meshing Roundtable

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