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Volumn 1, Issue , 2009, Pages 188-202
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Unsteady simulations of rotorcrafts in ground effect using a fast panel - Fast vortex formulation
a
ANSALDO ENERGIA
(Italy)
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Author keywords
[No Author keywords available]
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Indexed keywords
ADVANCE RATIO;
AGUSTA WESTLAND;
COMPUTATIONAL TIME;
COMPUTER MEMORIES;
EULERIAN;
FLIGHT REGIME;
FLOW RECIRCULATION;
FORWARD FLIGHT;
HOVERING ROTOR;
LIFTING SURFACES;
MAIN CHARACTERISTICS;
NAVIER-STOKES SOLVER;
NONLINEAR EFFECT;
NUMERICAL STUDIES;
PILOT WORKLOAD;
POTENTIAL TOOL;
RADIAL COMPONENT;
RECIRCULATIONS;
ROTOR DISKS;
ROTOR WAKE;
SMALL REGION;
SQUARE ROOTS;
UNSTEADY SIMULATIONS;
VORTICAL FLOWS;
WAKE VORTEX;
AIRCRAFT;
DISKS (STRUCTURAL COMPONENTS);
FREE FLIGHT;
GROUND EFFECT;
HELICOPTER SERVICES;
VORTEX FLOW;
WAKES;
HELICOPTER ROTORS;
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EID: 77952325688
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (8)
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References (22)
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