Dynamic wake models have developed over the years based on the desire to develop realistic rotorcraft response tools that could be used in various design and simulation applications. Early work concentrated on correlation with experimental data in both the frequency and time domain for rotors in hover and forward flight. More recent developments have extended these models to include effects of wake curvature and quasi-steady ground plane interactions. The most recent developments have focused on extension of these models to include all three components of flow velocity and not just on the rotor disk, the latter which could encompass applications to unsteady ground effect problems and mass injection at the rotor.
New developments in dynamics wake modeling for dynamics applications
Neue Entwicklungen bei der Berechnung des instationären Strömungsfeldes von Hubschrauberrotoren
Journal of the American Helicopter Society ; 48 , 2 ; 120-127
2003
8 Seiten, 10 Bilder, 21 Quellen
Article (Journal)
English
New Developments in Dynamic Wake Modeling for Dynamics Applications
Online Contents | 2003
|NEW DEVELOPMENTS IN DYNAMIC WAKE MODELING FOR DYNAMICS APPLICATIONS
British Library Conference Proceedings | 2001
|A Review of Wake Modeling Methods for Flight Dynamics Applications
British Library Conference Proceedings | 2009
|A review of rotorcraft wake modeling methods for flight dynamics applications
Tema Archive | 2009
|SAE Technical Papers | 1996
|