Acceleration techniques for an aeroelastic Euler method for a hovering rotor
- 1 March 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 33 (2) , 429-434
- https://doi.org/10.2514/3.46955
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Flap‐Lag Damping in Hover and Forward Flight with a Three‐Dimensional WakeJournal of the American Helicopter Society, 1993
- Effect of an Unsteady Three‐Dimensional Wake on Elastic Blade‐Flapping Eigenvalues in HoverJournal of the American Helicopter Society, 1993
- Transonic aeroelasticity analysis for rotor bladesJournal of Aircraft, 1992
- Hingeless Rotor Aeroelastic Stability Analysis with Refined Aerodynamic ModelingJournal of the American Helicopter Society, 1991
- Evaluation of a fourth-order compact operator scheme for Euler/Navier-Stokes simulations of a rotor in hoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Rotor Loads Prediction Utilizing a Coupled Aeroelastic Analysis with Refined Aerodynamic ModelingJournal of the American Helicopter Society, 1991
- Finite‐State Induced‐Flow Model for Rotors in Hover and Forward FlightJournal of the American Helicopter Society, 1989
- Iterative Lifting Surface Method for Thick Bladed Hovering Helicopter RotorsJournal of Aircraft, 1981
- Stability of Hingeless Rotor Blades in Hover with Pitch-Link FlexibilityAIAA Journal, 1977
- A Two-Dimensional Approximation to the Unsteady Aerodynamics of Rotary WingsJournal of the Aeronautical Sciences, 1957