Hybrid Computational-Fluid-Dynamics Platformto Investigate Aircraft Trailing Vortices
Author:
Affiliation:
1. University of Cape Town, Cape Town 7701, South Africa
2. Linköping University, 581 83 Linköping, Sweden
Funder
Department of Science and Technology (DST) and the National Research Foundation
AEROGUST project
National Aerospace Centre (NAC) of South Africa
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C035022
Reference29 articles.
1. Compressibility Effects of Extended Formation Flight
2. Navier-Stokes Simulations of Blade-Vortex Interaction Using High-Order-Accurate Upwind Schemes
3. Investigation of high-order upwinded differencing for vortex convection
4. An analysis of the performance of a high-order stabilised finite element method for simulating compressible flows
5. Review of summation-by-parts operators with simultaneous approximation terms for the numerical solution of partial differential equations
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