A zonal approach to solution of the Euler equations
Author:
Affiliation:
1. NASA, Ames Research Center, MoffettField, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-969
Reference29 articles.
1. Computation of the steady viscous flow over a tri-element 'augmentorwing' airfoil
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1. COMPUTATION OF TURBULENT TWO-PHASE FLOW ON OVERLAPPED GRIDS;Numerical Heat Transfer, Part B: Fundamentals;1997-09
2. Simulation and analysis of V-22 tiltrotor aircraft forward flight flowfield;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
3. The impact of computational zone interfacing on calculated scramjet performance;30th Aerospace Sciences Meeting and Exhibit;1992-01-06
4. Zonal Navier-Stokes methodology for flow simulation about a completeaircraft;Journal of Aircraft;1990-07
5. Navier-Stokes Computations About Complex Configurations Including a Complete F-16 Aircraft;Applied Computational Aerodynamics;1990-01-01
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