Engineering availability of aircrafts
, 2009 Engineering availability and operational readiness of an aircraft are requisites for its ability to operate. After the aircraft has been supplied, both features determine airworthiness of the aircraft, in compliance with the ARC (Airworthiness Review ...
Lewitowicz, J.
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Development Of A Control Flap For The Ultralight Helicopter [PDF]
, 2017 The purpose of this project is to develop control flap for ultralight helicopter based on the concept of changing the airflow. The structure of the control flap was analyzed based on the extreme condition. The control flap consists of two materials which
Zain, Mohammad Shair Mohd
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A Novel Framework for Qualification of a Composite-Based Main Landing Gear Strut of a Lightweight Aircraft. [PDF]
Polymers (Basel), 2023 Ahmad MA +4 more
europepmc +1 more source
The Basic Premises of EU Regulations Regarding the Safety of Unmanned Aircraft in the Context of their Development Process. [PDF]
J Intell Robot Syst, 2022 Kasprzyk P.
europepmc +1 more source
On the derivation and analysis of decision architectures for unmanned aircraft systems
, 2013 ©Cranfield University © BAE SystemsOperation of Unmanned Air Vehicles (UAVs) has increased significantly over the past few years. However, routine operation in non-segregated airspace remains a challenge, primarily due to nature of the environment and ...
Patchett, C H
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Certification of lightning protection for a full-authority digital engine control
, 1991 FADEC systems present many challenges to the lightning protection engineer. Verification of the protection-design adequacy for certification purposes presents additional challenges.
Dargi, M., Rupke, E., Wiles, K.
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Optimal Design and Testing of a Thermoplastic Pressurized Passenger Door Manufactured Using Thermoforming. [PDF]
Polymers (Basel), 2021 Růžek R +5 more
europepmc +1 more source
Tietojärjestelmä yleisilmailulentokoneiden jatkuvan lentokelpoisuusvalvonnan avuksi
, 2014 A software house Oy Fision Ltd decided to develop a custom information system to help in continuing airworthiness management of general aviation aircraft. The project was put in motion as a master’s thesis project by the author.
Kuokkanen, Jaakko
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Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy. [PDF]
Materials (Basel), 2022 Bednarz A +3 more
europepmc +1 more source
The Experimental Verification of Direct-Write Silver Conductive Grid and ARIMA Time Series Analysis for Crack Propagation. [PDF]
Sensors (Basel), 2021 Kurnyta A +5 more
europepmc +1 more source