Flowfield of a lifting rotor in hover - A Navier-Stokes simulation
- 1 October 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (10) , 2371-2378
- https://doi.org/10.2514/3.11236
Abstract
No abstract availableThis publication has 22 references indexed in Scilit:
- Rotor hover performance prediction using a free-wake, computational fluid dynamics methodJournal of Aircraft, 1989
- Solutions of the Navier‐Stokes Equations for the Flow About a Rotor BladeJournal of the American Helicopter Society, 1989
- Navier-Stokes calculations of hovering rotor flowfieldsJournal of Aircraft, 1988
- Numerical simulation of helicopter multi-bladed rotor flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Euler calculations for flowfield of a helicopter rotor in hoverJournal of Aircraft, 1987
- Euler solution of the transonic flow for a helicopter rotorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Conservative full-potential model for unsteady transonic rotor flowsAIAA Journal, 1987
- Solution of the unsteady Euler equations for fixed and rotor wing configurationsJournal of Aircraft, 1986
- Numerical solution of the full-potential equation for rotors and oblique wings using a new wake modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Solution method for a hovering helicopter rotor using the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985