Results 21 to 30 of about 4,521 (204)
Hangkong gongcheng jinzhan, 2018 With The rapid development of civil aircraft digital integrated collaborative development mode, the traditional airworthiness management system has become more and more unsuitable for the digitization, informatization and networking of the collaborative ...
He Jing +3 more
doaj +1 more source
Cailiao gongcheng, 2021 The single-lap joints with different overlap lengths were bonded by carbon fiber reinforced plastics (CFRP) laminate, and their failure load, fracture process and strain fields were characterized by digital image correlation (DIC) and universal testing ...
ZOU Tian-chun +4 more
doaj +1 more source
Hangkong gongcheng jinzhan, 2023 The civil aircraft flight deck door system is installed in the aircraft cabin to block the cockpit area and cabin area. In addition to providing normal access to the cockpit, it must have bullet proof and intrusion prevention functions to prevent non ...
MA Jun, LI Songze, ZHAO Xuwei
doaj +1 more source
Analysis on Airworthiness Special Conditions of Civil Helicopter Fly-by-wire Flight Control System
Hangkong gongcheng jinzhan, 2021 The advanced fly-by-wire flight control system can greatly improve the maneuverability and stability of civil helicopters, but this novel design also brings huge challenges to safety assessment.Traditional airworthiness standards may not fully cover the ...
MA Liqun, YANG Shibin, SHI Linxuan
doaj +1 more source
A Flexible Code Review Framework for Combining Defect Detection and Review Comments
Aerospace, 2023 Defects and errors in code are different in that they are not detected by editors or compilers but pose a potential risk to software operation. For safety-critical software such as airborne software, the code review process is necessary to ensure the ...
Xi Chen +5 more
doaj +1 more source
Sensors, 2021 The paper presents experimental verification of customized resistive crack propagation sensors as an alternative method for other common structural health monitoring (SHM) techniques.
Artur Kurnyta +5 more
doaj +1 more source
Numerical and Experimental UAV Structure Investigation by Pre-Flight Load Test
Sensors, 2020 This paper presents the preparation and execution of on-ground static and engine load tests for the composite unmanned aerial vehicle (UAV). The test was conducted for pre-flight structural strength verification of the remotely piloted aerial target ...
Artur Kurnyta +4 more
doaj +1 more source
Research on Type Design and Compliance Verification Method of ETOPS for Civil Aircraft Engine
Hangkong gongcheng jinzhan, 2022 Aircraft engine extended operations(ETOPS)eligibility is the basis for aircraft extended operations. In order to provide the guide for the domestic aircraft engine ETOPS type design and airworthiness compliance verification,the formation process of the ...
LI Haoran, LEI Yansheng, GONG Haowei
doaj +1 more source
Analysis of Single-Pilot Intention Modeling in Commercial Aviation
International Journal of Aerospace Engineering, 2023 With the continual enhancement of the onboard avionics, the minimum flight crew has been downsized from five to two-person crew mode, and reduced crew operation has drawn extensive attention from aviation experts.
Lei Dong +3 more
doaj +1 more source
Aerospace, 2023 Multi-fidelity surrogate modeling (MFSM) methods are gaining recognition for their effectiveness in addressing simulation-based design challenges. Prior approaches have typically relied on recursive techniques, combining a limited number of high-fidelity
Vinh Pham +3 more
doaj +1 more source