Results 21 to 30 of about 25,565 (312)
Influence of tilt angle and the number of guide vane blades towards the Savonius rotor performance
Additional guide vane (GV) to the Savonius rotor is used to overcome the low rotor efficiency. This study is experimentally carried out to know the influence of guide vane in improving two blades Savonius rotor performance.
Waled Yahya +5 more
doaj +1 more source
Four-Dimensional Gait Surfaces for a Tilt-Rotor—Two Color Map Theorem
This article presents the four-dimensional surfaces that guide the gait plan for a tilt-rotor. The previous gaits analyzed in the tilt-rotor research are inspired by animals; no theoretical base backs the robustness of these gaits.
Zhe Shen, Yudong Ma, Takeshi Tsuchiya
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Hurdle-Hop Simulation of Tilt-Rotor Aircraft Based on Optimal Control Theory
Aiming at simulating the hurdle-hop of tilt-rotor aircraft in forward flight near the ground, two models of numerical simulation and analysis based on optimal control theory were proposed.
doaj +1 more source
The numerical calculation model for the aero-acoustic analysis of a tilt rotor was established by combining the free wake method and the FW-H (Ffowcs Williams-Hawkings) equation.
YUAN Mingchuan +4 more
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To study the radar characteristics of the tiltrotor aircraft when considering rotor rotation and tilting actions, a dynamic calculation method (DCM) based on physical optics and physical theory of diffraction is presented. The results show that the radar
Zeyang Zhou +3 more
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The distributed electric tilt-rotor Unmanned Aerial Vehicle (UAV) combines the vertical take-off and landing (VTOL) capability of helicopters with the high-speed cruise performance of fixed-wing aircraft, offering a transformative solution for Urban Air ...
He Zhu +4 more
doaj +1 more source
EXPERIMENTAL VALIDATION OF TILT-ROTOR AERODYNAMIC PREDICTIONS
A comparison of experimental data with several numerical predictions of the aerodynamic loads on the ERICA model is presented. The calculations are carried out by several Partners of the NICETRIP consortium, with different codes, turbulence models and grids, with the objective of validating the predictive capability of the CFD tools.
J. Decours +5 more
openaire +4 more sources
Control and flight test of a tilt-rotor unmanned aerial vehicle
Tilt-rotor unmanned aerial vehicles have attracted increasing attention due to their ability to perform vertical take-off and landing and their high-speed cruising abilities, thereby presenting broad application prospects.
Chao Chen +3 more
doaj +1 more source
Aerodynamic Optimization Design of the Rotor Blade of a Tilt-rotor Aircraft
The aerodynamic design of tilt-rotor needs to synthetically consider the different requirements in helicopter mode and fixed-wing aircraft mode. The multi-objective genetic algorithm based on Kriging surrogate model is used to establish an optimization ...
Sun Kaijun +3 more
doaj +1 more source
Tilt-rotor multivariable attitude control with rotor state feedback
In this paper, a multi-objective optimization-based methodology for rotorcraft attitude control law design is applied to a tilt-rotor case; the framework allows to enforce requirements of stability, performance, control action moderation, and safety.
PANZA, SIMONE +3 more
openaire +2 more sources

