EROS — a common European Euler code for the analysis of the helicopter rotor flowfield
- 31 August 2000
- journal article
- review article
- Published by Elsevier BV in Progress in Aerospace Sciences
- Vol. 36 (5-6), 437-485
- https://doi.org/10.1016/s0376-0421(00)00006-3
Abstract
No abstract availableThis publication has 25 references indexed in Scilit:
- Elements of computational fluid dynamics on block structured grids using implicit solversProgress in Aerospace Sciences, 2000
- Performance prediction and flowfield analysis of rotors in hover, using a coupled Euler/boundary layer methodAerospace Science and Technology, 1999
- Euler Calculations of Multibladed Rotors in Hover by DLR and ONERA Methods and Comparison with Helishape TestsJournal of the American Helicopter Society, 1998
- Solution of the Unsteady Euler Equations Using an Implicit Dual-Time MethodAIAA Journal, 1998
- Implicit time-stepping methods for the Navier-Stokes equationsAIAA Journal, 1996
- Helicopter rotor blade computation in unsteady flows using moving overset gridsJournal of Aircraft, 1996
- Composite overlapping meshes for the solution of partial differential equationsJournal of Computational Physics, 1990
- Navier-Stokes calculations of hovering rotor flowfieldsJournal of Aircraft, 1988
- A general three-dimensional elliptic grid generation system on a composite block structureComputer Methods in Applied Mechanics and Engineering, 1987
- Solution of the unsteady Euler equations for fixed and rotor wing configurationsJournal of Aircraft, 1986