Improved Iteration Algorithm for Nonlinear Vortex Lattice Method
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.44829
Reference13 articles.
1. Extension of a Vortex-Lattice Method to Include the Effects ofLeading-Edge Separation
2. Nonlinear Prediction of Aerodynamic Loads on Lifting Surfaces
3. Calculation of symmetric vortex separation affecting subsonic bodiesat high incidence
4. Numerical calculation of nonlinear aerodynamics of wing-body configurations
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