Results 51 to 60 of about 416,763 (296)

Ultra‐Improved Interfacial Strength Between Metallic Surface and Polyurethane via Cost‐Effective Anodizing Process

open access: yesAdvanced Materials Interfaces, EarlyView.
SAA significantly enhanced Al/PU bonding, increasing SLSS by up to 920% and fracture energy by 15 100% through optimized micro‐nano porous surfaces. RSM identified the optimal anodizing conditions, while ML confirmed sulfuric acid concentration and roughness as dominant predictors of strength.
Umut Bakhbergen   +6 more
wiley   +1 more source

The microstructure and mechanical properties of TA15 joints by laser forming connection

open access: yesInternational Journal of Lightweight Materials and Manufacture, 2018
The microstructure and mechanical properties of laser forming connected joints of TA15 fabricated by hot isostatic pressing (HIP) process were investigated. The results showed that high-quality joints are produced by laser forming connection (LFC).
Bendong Xing   +4 more
doaj   +1 more source

Flying car design and testing [PDF]

open access: yes, 2009
This paper is primarily concerned with the inverted design process and manufacture of a flying car prototype which can overcome the problem of traffic management in the world today.
Klein, S., Smrcek, L.
core  

Energy Consumption Optimization in Trajectory Planning for Fuel Cell Hybrid Uavs Based On HMPC

open access: yesAdvanced Robotics Research, EarlyView.
The endurance limitation of multirotor drones is a critical challenge. This study adopts a hybrid power system of fuel cells and lithium‐ion batteries. Using Nondominated Sorting Genetic Algorithm II, it integrates trajectory planning with energy management optimization.
Xindi Wang   +7 more
wiley   +1 more source

Analysis method of flight crew human factors in system safety assessment

open access: yesHangkong gongcheng jinzhan
With the improvement of high complexity and automation level of the aircraft systems,pilots are often ill-prepared to cope with an actual emergency or failure,and their corrective actions may be erroneous,delayed or incomplete.
LIU Huixing   +3 more
doaj   +1 more source

Comparison of closed loop model with flight test results [PDF]

open access: yes, 1981
An analytic technique capable of predicting the landing characteristics of proposed aircraft configurations in the early stages of design was developed.
George, F. L.
core   +1 more source

Collision‐Resilient Winged Drones Enabled by Tensegrity Structures

open access: yesAdvanced Robotics Research, EarlyView.
Based on structures of birds such as the woodpeck, this article presents the collision‐resilient aerial robot, SWIFT. SWIFT leverages tensegrity structures in the fuselage and wings which allow it to undergo large deformations in a crash, without sustaining damage. Experiments show that SWIFT can reduce impact forces by 70% over conventional structures.
Omar Aloui   +5 more
wiley   +1 more source

Calculation Analysis on the Door’s Contact Force of theFlight Lock Mechanism for Civil Airplane

open access: yesHangkong gongcheng jinzhan, 2018
It is of great significance to study the contact force in the aircraft’s flight lock mechanism for the design of the flight lock mechanism of the civil aircraft. The function and main design basis of flight lock are firstly introduced.
Liu Chengye, Huang Zhenting, Zhou Ying
doaj   +1 more source

A Degradable Bioinspired Flier with Aerogel‐Based Colorimetric Sensors for Environmental Monitoring

open access: yesAdvanced Science, EarlyView.
Biodegradable fliers are developed inspired by Tipuana tipu samaras, integrating cellulose nanocrystal aerogel (CNCa) sensors loaded with natural dyes for pH and ammonia detection. The lightweight, degradable fliers mimic natural morphology and aerodynamics, offering an eco‐friendly, scalable solution for in situ environmental monitoring after passive ...
Gianpaolo Gallo   +4 more
wiley   +1 more source

Effect of rolling texture on bearing capacity of aircraft repair patches and replaced panels

open access: yesAviation
The article combines issues related to biaxial fatigue loading, corrections for equivalent stress calculations, and the practical application of new knowledge regarding biaxial fatigue in the aviation industry.
Mykhailo Karuskevych   +3 more
doaj   +1 more source

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