Anovel Wake Interference Model For Helicopter Real-Time Simulation

Simple item page
dc.contributor.authorÐeverlija, J.
dc.contributor.authorAbà, A.
dc.contributor.authorCapone, P.
dc.contributor.authorMasi, A.
dc.contributor.authorDaniele, M.
dc.contributor.authorScorcelletti, F.
dc.date.accessioned2026-08-13T14:17:21Z
dc.date.issued2024
dc.description.abstractAerodynamic mutual interference occurring between rotors’ wake, fuselage and aerodynamic surfaces has a notable impact on the flight characteristics of a helicopter. A simple and flexible method for quantifying aerodynamic interaction between the rotor wake and airframe is presented. The model, implemented in the Zurich University of Applied Sciences (ZHAW) simulation framework, has been developed for both off-line and real-time helicopter simulation and was validated by compar-ison against an existing model already validated with flight test data. The model was also tested on the motion-based, virtual-reality flight simulator ZHAW High-Fidelity Simulator.
dc.identifier.citationPresented at 50th European Rotorcraft Forum (ERF 2024), September 10-12, 2024, Marseille, France.
dc.identifier.urihttps://hdl.handle.net/20.500.11881/4567
dc.language.isoen
dc.titleAnovel Wake Interference Model For Helicopter Real-Time Simulation

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
DocFinal-139.pdf
Size:
1.31 MB
Format:
Adobe Portable Document Format
Download

Collections

Papers