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The inverted V-tail is equipped in a twin-boom UAV,whose intersection angle can influence the aerodynamic characteristics and static stability. A twin-boom UAV with inverted V-tail is proposed,and compared with the U-tail configuration by numerical ...
WANG Xiaolu +3 more
doaj +1 more source
Investigating Planar and Nonplanar Wing Planform Optimisation for Ground Effect Aircraft
Wing-in-Ground (WIG) effect aircraft are gaining attention for their potential in reducing environmental impact. However, optimising wing planforms based solely on aerodynamics might improve performance while compromising static height stability of WIG ...
Rejish Jesudasan +2 more
doaj +1 more source
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions
The recent improvement of technology readiness level in aeronautics and the renewed demand for faster transportation are driving the rebirth of supersonic flight for commercial aviation.
Andrea Aprovitola +3 more
doaj +1 more source
Prediction of Wing Downwash Using CFD [PDF]
Wing downwash study and estimation of downwash effect on the tail plane is an important task during the aircraft design process, although a lot of papers and works has been done, but the experimental work is the most important, the progress in CFD ...
Mohammed MAHDI
doaj +1 more source
Numerical Analysis of Bioinspired Tails in a Fixed-Wing Micro Air Vehicle
Bird tails play a key role in aerodynamics and flight stability. They produce extra lift for takeoff and landing maneuvers, enhance wing functions and maintain stability during flight (keeping the bird from yawing, rolling and pitching, or otherwise ...
Estela Barroso Barderas +3 more
doaj +1 more source
Factors affecting static longitudinal stability and control [PDF]
Donlan, C. J.
core +2 more sources
Aerodynamic Simulation of a Tactical Aerostat and Evaluating the Longitudinal Static Coefficients [PDF]
In this paper, the computational fluid dynamics simulation of a tactical aerostat is conducted and the longitudinal static coefficients of the aerostat are evaluated.
Ali Jafarian +2 more
doaj +1 more source
Two-Way Coupled Aero-Structural Optimization of Stable Flying Wings
An aero-structural algorithm to optimize a flying wing in cruise conditions for preliminary design is developed using two-way interaction between the structure and aerodynamics.
José D. Hoyos +5 more
doaj +1 more source
Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose [PDF]
The purpose of this paper is to construct a new general vehicle model as an open fundamental material for the guidance and control research. In this study, parameterized configuration, aerodynamics calculation, control-oriented modeling, stability ...
Jun Huang +4 more
doaj +2 more sources
In recent years, due to the disadvantages of poor overall performance and low safety reserve, there are more and more reinforcement cases for the bridge deck system of long-span arch bridges under the stress of beams.
Chaowei Hao +4 more
doaj +1 more source

