-
1
Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft
Published 2023-11-01“…Through the kinematic and aerodynamic coupling analysis of the combined mechanism, the coupling dynamic characteristics of the flapping-wing aircraft are obtained, which provides a research basis for the flight control and performance improvement of the flapping-wing aircraft in the future.…”
Get full text
Article -
2
-
3
Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust
Published 2019-01-01Get full text
Article -
4
-
5
Structural Design and Experiment Analysis of a Morphing Wing Structure
Published 2020-03-01“…The optimization algorithm is used to optimize the morphing wing structure. On the basis of theoretical research, the experimental prototype is processed and the related experimental tests are carried out.…”
Get full text
Article -
6
Analysis of clogging factors in single-wing labyrinth drip irrigation tape.
Published 2024-01-01“…In this paper, we designed a uniform orthogonal test to study the effects of fertilizer concentration, sediment content and working pressure on the clogging of single-wing labyrinth drip irrigation tapes. The observed data from the experiment were analysed and calculated using range analysis, variance analysis, and main-effect multiple comparison analysis, then the optimal working conditions were determined. …”
Get full text
Article -
7
Control Characteristics Analysis of Multi-Section Morphing Wing Based on Centroid Self-Trimming
Published 2025-01-01“…Based on the research on the sweep angle change of the elbow and hand wing sections during the flight of large birds, this paper proposes a multi-section variable-sweep wing structure suitable for large-scale UAVs. …”
Get full text
Article -
8
Analysis and design of a fixed wing unmanned aerial vehicle gas launching system
Published 2025-02-01Get full text
Article -
9
Geometrical Nonlinear Aeroelastic Stability Analysis of a Composite High-Aspect-Ratio Wing
Published 2008-01-01“…Planar doublet lattice method is used to calculate unsteady aerodynamics in frequency domain ignoring the bending effect of the deflected wing. And then, the aeroelastic stability analysis of the system under a given load condition is successively carried out. …”
Get full text
Article -
10
Design of Variable Amplitude Flapping Wing Aircraft and Realization of Multiple Flight Modes
Published 2021-05-01Get full text
Article -
11
Fatigue Experiment and Failure Mechanism Analysis of Aircraft Titanium Alloy Wing–Body Connection Joint
Published 2024-12-01“…Taking the titanium alloy wing–body connection joint at the rear beam of a certain type of aircraft as the research object, this study analyzed the failure mechanism and verified the structural safety of the wing–body connection joint under actual flight loads. …”
Get full text
Article -
12
UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT
Published 2017-01-01“…In order to study the parameters of a folding wing‘s spreading performance which is used on the guided missile’s actuator,the unfolding performance was researched. …”
Get full text
Article -
13
DYNAMICS ANALYSIS AND LIGHTWEIGHT DESIGN OF BIONIC ROBOTIC FISH FRAME MECHANISM (MT)
Published 2023-01-01“…The caudal fin mechanism was introduced into ADAMS environment for dynamic analysis, and the motion load of the bionic robotic fish frame mechanism was obtained. …”
Get full text
Article -
14
Development of Anisogrid Lattice Composite Structures for Fighter Wing Applications
Published 2024-01-01“…This paper presents research on the use of anisogrid lattice structures in fighter wing applications. …”
Get full text
Article -
15
Design and Aerodynamic Analysis of a Flapping Mechanism for Foldable Biomimetic Aircraft
Published 2025-01-01Get full text
Article -
16
Conceptual Design of an Unmanned Fixed-Wing Aerial Vehicle Based on Alternative Energy
Published 2019-01-01“…In fact, the aerodynamic analysis is obtained for a preliminary design; this step involves the wing, fuselage, and empennage of the UAV. …”
Get full text
Article -
17
The Lift Enhancement Effect of a New Fluidic Oscillator on High-Lift Wings
Published 2025-01-01Get full text
Article -
18
Computational assessment of winglet-induced variations in pressure coefficients on NACA 4418 aircraft wings
Published 2025-01-01“…This study presents a computational analysis of the effects of winglets on the aerodynamic performance of NACA 4418 aircraft wings, focusing on the variations in pressure coefficients. …”
Get full text
Article -
19
-
20
Design and fabrication study of a small remote-controlled bionic butterfly flapping-wing flying machine
Published 2024-12-01“… This research is devoted to simulating the flight characteristics of real butterflies, and a small remote-controlled bionic butterfly flying machine is designed and manufactured. …”
Get full text
Article