Results 21 to 30 of about 1,422,313 (180)
The paper presents the results of a numerical simulation of the flow and acoustic field generated by the PZL W3-A “Sokół” (Falcon) helicopter main rotor in high-speed forward flight conditions based on the URANS approach and the chimera overlapping ...
OSKAR SZULC +4 more
doaj +1 more source
Modelling the helicopter rotor aerodynamics at forward flight with free wake model and URANS method
The presented work is dedicated to the numerical study of the aerodynamic characteristics of the helicopter rotor. Two approaches to modeling of the rotor are applied: the free wake model developed by the Authors with using steady airfoil characteristics
Yuri Ignatkin +3 more
doaj +1 more source
Propeller ground and ceiling effect in forward flight
Click on the DOI link to access this article at the publishers website (may not be free).The study of the fixed-pitch small-scale propeller in ground/ceiling effect is extended to forward flight conditions.
Cai, Jielong, Gunasekaran, Sidaard
core +1 more source
A Numerical Study of the Sound and Force Production of Flexible Insect Wings
We numerically solved the acoustic and flow field around cicada wing models with parametrically varied flexibility using the hydrodynamic/acoustic splitting method. We observed a gradual change of sound directivity with flexibility.
Biao Geng +4 more
doaj +1 more source
Mathematical modeling and investigating the effect of the area of the horizontal stabilizer on the stability of a single-main-rotor helicopter in forward flight [PDF]
This paper investigates the effect of the area of the horizontal stabilizer of a single-main-rotor helicopter on its dynamic responses, stability properties, and flight handling quality during forward flights.
Fatemeh Ghaderi, Farid Shahmiri
doaj +1 more source
Optimised Tuning of a PID-Based Flight Controller for a Medium-Scale Rotorcraft
This paper presents the parameter optimisation of the flight control system of a singlerotor medium-scale rotorcraft. The six degrees-of-freedom (DOF) nonlinear mathematical model of the rotorcraft is developed.
Lindokuhle J. Mpanza +1 more
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Helicopters are more and more widely used for water dumping in fire extinguishing operations nowadays. Increasing attention is being paid to improving helicopter firefighting efficiency.
Tejun Zhou +3 more
doaj +1 more source
Flight test: Supporting the investigation of factors affecting loss of control of light aircraft [PDF]
A quarter of all fatal General Aviation accidents in the UK during the period 1980 to 2006 involved Loss of Control (LoC) in Visual Meteorological Conditions (VMC).
Gratton, GB, Bromfield, MA
core +6 more sources
Aerodynamic analysis of toroidal propellers in forward flight [PDF]
Research is being conducted to develop a new generation of propellers that can enable quieter and more efficient flight. One promising development in this area are Toroidal propellers, for which the blades are shaped as a closed loop.
Oliviu SUGAR-GABOR +2 more
doaj +1 more source
Transient Thrust Analysis of Rigid Rotors in Forward Flight
The purpose of this study was to investigate and quantify the transient thrust response of two small rigid rotors in forward flight. This was accomplished using a distributed doublet-based potential flow method, which was validated against wind-tunnel ...
Travis Krebs +2 more
doaj +1 more source

