Numerical study of vortex-dominated flows for wings at high incidence and sideslip
Author:
Affiliation:
1. ViGYAN, Inc., Hampton, Virginia 23666
2. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46175
Reference20 articles.
1. Preconditioned methods for solving the incompressible and low speed compressible equations
2. Implicit Finite-Difference Procedures for the Computation of Vortex Wakes
3. Evaluation of preconditioning methods for time-marching systems
4. A numerical method for solving incompressible viscous flow problems
5. Computation of inviscid incompressible flow with rotation
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2. Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration;Journal of Aircraft;2016-01
3. Turbulence models for the computation of flow past airplanes;Progress in Aerospace Sciences;1997-01
4. Computational study of a turbulent delta-wing flowfield using two-equation turbulence models;Fluid Dynamics Conference;1996-06-17
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