Sliding mesh algorithm for CFD analysis of helicopter rotor–fuselage aerodynamics
- 18 February 2008
- journal article
- research article
- Published by Wiley in International Journal for Numerical Methods in Fluids
- Vol. 58 (5), 527-549
- https://doi.org/10.1002/fld.1757
Abstract
No abstract availableKeywords
This publication has 15 references indexed in Scilit:
- CFD Analysis of Rotor-Fuselage Interactional AerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2007
- Simulation of Unsteady Rotor-Fuselage Aerodynamic Interaction Using Unstructured Adaptive MeshesJournal of the American Helicopter Society, 2006
- A framework for CFD analysis of helicopter rotors in hover and forward flightInternational Journal for Numerical Methods in Fluids, 2006
- Simulation of Unsteady Rotor Flow Field Using Unstructured Adaptive Sliding MeshesJournal of the American Helicopter Society, 2004
- Aeroelastic Analysis of Helicopter Rotor Blades on Deformable Chimera GridsJournal of Aircraft, 2004
- A fully distributed unstructured Navier-Stokes solver for large-scale aeroelasticity computationsThe Aeronautical Journal, 2001
- A relaxation approach to patched-grid calculations with the euler equationsJournal of Computational Physics, 1986
- A conservative treatment of zonal boundaries for euler equation calculationsJournal of Computational Physics, 1986
- Upwind schemes and boundary conditions with applications to Euler equations in general geometriesJournal of Computational Physics, 1983
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981