Results 21 to 30 of about 12,466 (308)
Numerical study on aerodynamics of banked wing in ground effect
Unlike conventional airplane, a WIG craft experiences righting moment and adverse yaw moment in banked turning in ground effect. Numerical simulations are carried out to study the aerodynamics of banked wing in ground effect.
Qing Jia, Wei Yang, Zhigang Yang
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Aerodynamic improvement of a delta wing in combination with leading edge flaps
Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been reported from wide range points of view. The aim of this study is to research the aerodynamic improvement of delta wing in low Reynold’s number region to ...
Tadateru Ishide, Mao Itazawa
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The article explores the possibility of improving the aerodynamic properties of a supercritical-airfoil wing, typical for a modern passenger aircraft, using delta planform passive devices of large relative areas, installed along the leading edge at the ...
D. Gueraiche, S. А. Popov
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Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 1: Methodology and analysis [PDF]
The essence of this two-part paper is the analytical, aerodynamic modelling of insect-like flapping wings in the hover for microair vehicle applications.
Knowles, Kevin +2 more
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In this paper, we describe new annular examples of complete translating solitons for the mean curvature flow and how they are related to a family of translating graphs, the $\Delta$-wings. In addition, we will prove several related results that answer questions that arise naturally in this investigation.
Hoffman, David +2 more
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Aerodynamics of Reverse Delta Wing
Delta wings are mostly used in supersonic jets and fighter aircrafts. A delta wing is naturally stable and produces vortex lift, so the flow separation can be made into increasing lift. This augmented lift comes at an expense of high drag. A reverse delta wing is nothing but an inverted delta wing, the forward swept wings were inspired from this design.
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Unsteady Characteristics of Breakdown Vortices over Delta Wing [PDF]
Experiment of unsteady pressure measurement on the surface of wing with 75° sweep delta wing has been carried out in a wind tunnel in order to investigate unsteady characteristics of breakdown vortices over delta wing after the leading edge vortices were
Zhi Yong Lu +3 more
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Aerodynamic Characteristics Of A Flat Plate Delta Wing With Deflected Wing Tips [PDF]
The low-speed aerodynamic characteristics of a novel flat plate delta wing with deflected wing tips is the focus of this study. The motivation for this project is to explore the high maneuverability capabilities of delta wings for autonomous unmanned ...
Whitfield, Clifford A. +3 more
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DYE VISUALIZATION OF A YAWED SLENDER DELTA WING
In the present experimental study, effects of yaw angle, β on the flow structure at high angles of attack, α with 70° sweep angle, Λ were investigated using the dye visualization technique. In the case of zero yaw angle, β a pair of leading edge vortices take place on both sides of cords axis are more or less symmetrical over the delta wing.
Karasu, Ilyas +3 more
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Vortex Flow and Aerodynamic Performance of a Reverse Delta Wing [PDF]
The unsteady flow past a reverse delta wing is simulated numerically to characterize the structure of the vortical flow and associated unsteady phenomena, and quantify the impact of such structures on the aerodynamic performance.
Cortelezzi, Luca +3 more
core +1 more source

