Navier-Stokes computation of wing/rotor interaction for a tilt rotor in hover
- 1 November 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (11), 2595-2603
- https://doi.org/10.2514/3.11272
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Unsteady shock-vortex interaction on a flexible delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Calculations of the flow past bluff bodies, including tilt-rotor wing sections at alpha = 90 degPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Unsteady aerodynamic simulation of multiple bodies in relative motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Navier-Stokes simulation of transonic flow over wing-fuselage combinationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Practical applications of new LU-ADI scheme for the three-dimensional Navier-Stokes computation of transonic viscous flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Multi-dimensional formulation of CSCM - An upwind flux difference eigenvector split method for the compressible Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981
- A diagonal form of an implicit approximate-factorization algorithmJournal of Computational Physics, 1981
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAIAA Journal, 1980
- Conservation equations of gasdynamics in curvilinear coordinate systemsJournal of Computational Physics, 1974