Euler calculations for multielement airfoils using Cartesian grids
Author:
Affiliation:
1. North Carolina State University, Raleigh, NC
2. NASA, Langley Research Center, Theoretical Aerodynamics Branch, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-291
Reference12 articles.
1. Boundary-fitted coordinate systems for numerical solution of partial differential equations—A review
2. Progress in Finite-Volume Calculations for Wing-Fuselage Combinations
3. Prediction of critical Mach number for store configurations
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