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Document type:
Konferenzbeitrag 
Author(s):
Bludau J.,Rauleder J.,Hajek M. 
Title:
Validation of a Dynamic Inflow Model Based on a Flight Dynamics Model and a Lattice-Boltzmann Fluid Solver Using Flight Test Data 
Pages contribution:
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...    »
 
Keywords:
Rotorcraft Inflow Flight Test Real-time 
Dewey Decimal Classification:
620 Ingenieurwissenschaften 
Book / Congress title:
43th European Rotorcraft Forum, Milan 
Organization:
Leonardo Helicopters 
Year:
2017 
Covered by:
Scopus