Numerical solutions of forward-flight rotor flow using an upwind method
- 1 June 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (6) , 374-380
- https://doi.org/10.2514/3.46037
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Upwind algorithm for the parabolized Navier-Stokes equationsAIAA Journal, 1989
- Numerical simulation of underexpanded plumes using upwind algorithmsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Numerical simulation of helicopter multi-bladed rotor flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Navier-Stokes computations of prolate spheroids at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Lower-upper implicit schemes with multiple grids for the Euler equationsAIAA Journal, 1987
- An Euler solver for calculating the flowfield of a helicopter rotor in hover and forward flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Euler solution of the transonic flow for a helicopter rotorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Computation of rotor blade flows using the Euler equationsJournal of Aircraft, 1986
- Solution of the unsteady Euler equations for fixed and rotor wing configurationsJournal of Aircraft, 1986
- Euler solver for three-dimensional supersonic flows with subsonic pocketsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985