Results 151 to 160 of about 1,426,014 (374)

In‐flight glycaemic control using automated insulin delivery systems: A within‐subject comparative pilot study

Diabetes, Obesity and Metabolism, EarlyView.
Abstract Background Automated insulin delivery systems (AID) are increasingly used by people living with type 1 diabetes, but their functionality during air travel remains insufficiently studied. Some concerns have arisen regarding safety using AID systems under flight conditions, particularly related to potential insulin delivery errors induced by ...
Renald Meçani, Silvia Basta, Petra M. Baumann, Monika Cigler, Omaima el Hakouni, Daniel A. Hochfellner, Fariba Shojaee‐Moradie, Ka Siu Fan, Dietrich Tews, Thomas R. Pieber, David Russell‐Jones, Chantal Mathieu, Gerd Koehler, Julia K. Mader   +13 more
wiley   +1 more source

The Leading Edge 250: Oblique wing aircraft configuration project, volume 4 [PDF]

The design of a high speed transport aircraft using the oblique wing concept as a part of the High Speed Civil Transport (HSCT) aircraft study is the Leading Edge 250 capable of travelling at Mach 4 with 250 passengers and has a 6,500 nautical mile range.
Moore, Peri, Nguyen, Dan, Oganesyan, Petros, Palmer, Charles, Schmidt, Andre   +4 more
core   +1 more source

Vehicle for civil helicopter ride quality research [PDF]

, 1975
A research aircraft for investigating the factors involved in civil helicopter operations was developed for NASA Langley Research Center. The aircraft is a reconfigured 17000 kg (36000 lb) military transport helicopter.
Schlegel, R. G., Snyder, W. J.
core   +1 more source

Performance of continuous glucose monitoring systems (CGMs) during commercial flights in T1DM: A within‐subject comparative pilot study

Diabetes, Obesity and Metabolism, EarlyView.
Abstract Aims Continuous glucose monitoring (CGM) systems are increasingly used, but their accuracy under flight‐conditions remains insufficiently studied. We assessed sensor accuracy of four CGMs during in‐flight (mid‐haul) and ground conditions.
Renald Meçani, Silvia Basta, Petra M. Baumann, Monika Cigler, Omaima El Hakouni, Daniel A. Hochfellner, Fariba Shojaee‐Moradie, Ka Siu Fan, Dietrich Tews, Thomas R. Pieber, David Russell‐Jones, Chantal Mathieu, Gerd Koehler, Julia K. Mader, EASA Diabetes Consortium   +14 more
wiley   +1 more source

A hybrid deep neural network based on multi-time window convolutional bidirectional LSTM for civil aircraft APU hazard identification

, 2021
Di Zhou, Zhuang Xiao, Hongfu Zuo
semanticscholar   +1 more source

Civil aircraft and aircraft engines : 2004 [PDF]

, 2005
Current industrial report.

core  

Fatigue Crack Nucleation and Growth in Recrystallized Annealed Ti‐6Al‐4V Combat Aircraft Structures

Fatigue &Fracture of Engineering Materials &Structures, EarlyView.
ABSTRACT In the Swiss Air Force (SAF) F/A‐18C/D Hornet fleet, recrystallized annealed Ti‐6Al‐4V was selected for the wing carry through bulkheads to meet their demanding operational usage profile requirements that included increased airframe strength and toughness.
I. Field, B. Main, M. Jones, S. Barter, R. F. do Rosario, M. Figliolino   +5 more
wiley   +1 more source

Fatal Civil Aircraft Accidents [PDF]

Pathology, 1971
openaire   +2 more sources

Autonomous Ground Refuelling Approach for Civil Aircrafts using Computer Vision and Robotics [PDF]

, 2021
Suleyman Yildirim, Zeeshan A. Rana, Gilbert Tang   +2 more
openalex   +1 more source

Calculated performance, stability and maneuverability of high-speed tilting-prop-rotor aircraft [PDF]

The feasibility of operating tilting-prop-rotor aircraft at high speeds is examined by calculating the performance, stability, and maneuverability of representative configurations. The rotor performance is examined in high-speed cruise and in hover.
Bowles, Jeffrey V., Johnson, Wayne, Lau, Benton H.   +2 more
core   +1 more source