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Dokumenttyp:
Konferenzbeitrag 
Autor(en):
Bludau J.,Rauleder J.,Hajek M. 
Titel:
Validation of a Dynamic Inflow Model Based on a Flight Dynamics Model and a Lattice-Boltzmann Fluid Solver Using Flight Test Data 
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 an...    »
 
Stichworte:
Rotorcraft Inflow Flight Test Real-time 
Kongress- / Buchtitel:
43th European Rotorcraft Forum, Milan 
Ausrichter der Konferenz:
Leonardo Helicopters 
Jahr:
2017