Computation of the steady viscous flow over a tri-element 'augmentorwing' airfoil
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-21
Reference14 articles.
1. The transonic multi-foil Augmentor-Wing
2. Automatic mesh-point clustering near a boundary in grid generation with elliptic partial differential equations
3. Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries
Cited by 3 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. Investigation of blending-function-based overlapping-grid technique for compressible flows;Computer Methods in Applied Mechanics and Engineering;2001-07
2. Euler calculations for wings using Cartesian grids;25th AIAA Aerospace Sciences Meeting;1987-03-24
3. A zonal approach to solution of the Euler equations;3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference;1982-06-07
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