Adaptive Grid Sequencing and Interpolation Schemes for Helicopter Rotor Wake Analyses
- 1 September 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 36 (9), 1593-1602
- https://doi.org/10.2514/2.585
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
- Challenges in Understanding the Vortex Dynamics of Helicopter Rotor WakesAIAA Journal, 1998
- Free-Wake Analysis of Tandem, Tilt-Rotor and Coaxial Rotor ConfigurationsJournal of the American Helicopter Society, 1996
- Evaluation of a Navier‐Stokes Analysis Method for Hover Performance PredictionJournal of the American Helicopter Society, 1996
- Rotor free-wake modeling using a pseudoimplicit relaxation algorithmJournal of Aircraft, 1995
- A Finite‐Volume Euler Solver for Computing Rotary‐Wing Aerodynamics on Unstructured MeshesJournal of the American Helicopter Society, 1993
- Direct Periodic Solutions of Rotor Free Wake CalculationsJournal of the American Helicopter Society, 1993
- Efficient Free Wake Calculations Using Analytical/Numerical MatchingJournal of the American Helicopter Society, 1993
- Solutions of the Navier‐Stokes Equations for the Flow About a Rotor BladeJournal of the American Helicopter Society, 1989
- Vortex theory for hovering rotorsAIAA Journal, 1982
- A Computer Model for the Evaluation of Helicopter Fire Control SystemsJournal of the American Helicopter Society, 1970