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Titel:

Validation of a Dynamic Inflow Model Based on a Flight Dynamics Model and a Lattice-Boltzmann Fluid Solver Using Flight Test Data

Dokumenttyp:
Konferenzbeitrag
Autor(en):
Bludau J.,Rauleder J.,Hajek M.
Seitenangaben Beitrag:
12
Abstract:
A fully-coupled, real-time-capable fluid dynamics/flight dynamics simulation was developed, that is validated against flight test data measured with a MBB Bo-105 helicopter. The highly-efficient Lattice- Boltzmann based fluid dynamics solver and the blade element based flight dynamics code were coupled through the rotor thrust and inflow. This dynamic inflow model extracted the inflow velocities from the computed flow field and passed them to the flight dynamics code to predict thrust and ro...     »
Stichworte:
Rotorcraft Inflow Flight Test Real-time
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
43th European Rotorcraft Forum, Milan
Ausrichter der Konferenz:
Leonardo Helicopters
Jahr:
2017
Nachgewiesen in:
Scopus
 BibTeX