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Journal articles on the topic 'Commercial aircraft'

Author: Grafiati

Published: 4 June 2021

Last updated: 26 July 2025

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1

Fujita, Etsushi, Taichi Higashioka, Manabu Sugiura, and Osamu Kohashi. "Evaluation method of military aircraft noise using AI analysis of aircraft images." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 263, no. 6 (2021): 854–62. http://dx.doi.org/10.3397/in-2021-1668.

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In recent aircraft noise survey in Japan, noise data is associated with each aircraft by flight log or by radio information including transponder signals. Especially, above Tokyo metropolitan area, flight tracks are tangled extremely each other, therefore assessments from various perspectives such as departure / arrival airport, used runway, aircraft model, and operator have been demanded for determining noise policies. However, for military aircrafts, it is not easy to identify their information with the same way as commercial aircrafts, because their flight logs are not disclosed and many of

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2

Bagshaw, M. "Commercial aircraft cabin altitude." Journal of the Royal Society of Medicine 100, no. 2 (2007): 64. http://dx.doi.org/10.1258/jrsm.100.2.64-a.

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3

Gerz, Thomas, Frank Holzäpfel, and Denis Darracq. "Commercial aircraft wake vortices." Progress in Aerospace Sciences 38, no. 3 (2002): 181–208. http://dx.doi.org/10.1016/s0376-0421(02)00004-0.

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4

Bagshaw, Michael. "Commercial aircraft cabin altitude." Journal of the Royal Society of Medicine 100, no. 2 (2007): 64. http://dx.doi.org/10.1177/014107680710000207.

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5

Nangia, R. K. "Efficiency parameters for modern commercial aircraft." Aeronautical Journal 110, no. 1110 (2006): 495–510. http://dx.doi.org/10.1017/s0001924000001391.

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Abstract Currently, there is great emphasis, worldwide, on environmental issues. This will have an impact on civil aircraft design, manufacture and operation. Since the advent of the jet engine and swept wing aircraft, the trends have naturally tended towards greater productivity through increasing speed and payload. The cruise speed of conventional civil aircraft is unlikely to increase beyond current levels. Further increases in productivity are achieved by increasing payloads. This has led towards larger aircraft with the capability for increased ranges. It is shown that designing aircraft

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6

Longmuir, Mark, and N. A. Ahmed. "Commercial Aircraft Exterior Cleaning Optimization." Journal of Aircraft 46, no. 1 (2009): 284–90. http://dx.doi.org/10.2514/1.38472.

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7

Eberl, F., S. Gardiner, G. Campanile, G. Surdon, M. Venmans, and P. Prangnell. "Ageformable panels for commercial aircraft." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 222, no. 6 (2008): 873–86. http://dx.doi.org/10.1243/09544100jaero290.

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8

Page, Richard L., Mohamed H. Hamdan, and David K. McKenas. "Defibrillation Aboard a Commercial Aircraft." Circulation 97, no. 15 (1998): 1429–30. http://dx.doi.org/10.1161/01.cir.97.15.1429.

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9

Taylor, G. C., R. D. Bentley, N. A. Horwood, et al. "TEPC measurements in commercial aircraft." Radiation Protection Dosimetry 110, no. 1-4 (2004): 381–86. http://dx.doi.org/10.1093/rpd/nch229.

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10

Rodenberg, Howard. "Medical emergencies aboard commercial aircraft." Annals of Emergency Medicine 16, no. 12 (1987): 1373–77. http://dx.doi.org/10.1016/s0196-0644(87)80422-5.

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11

Breugelmans, J. Gabrielle, Phillip Zucs, Klaudia Porten, et al. "SARS Transmission and Commercial Aircraft." Emerging Infectious Diseases 10, no. 8 (2004): 1502–3. http://dx.doi.org/10.3201/eid1008.040093.

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12

Jackson, Scott. "SYSTEMS ENGINEERING FOR COMMERCIAL AIRCRAFT." INCOSE International Symposium 7, no. 1 (1997): 36–43. http://dx.doi.org/10.1002/j.2334-5837.1997.tb02151.x.

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13

Zhang, Yongjie, Kang Cao, Ke Liang, and Yongqi Zeng. "Study on the evaluation model of serialized civil aircraft commonality index based on fuzzy set theory." Journal of Intelligent & Fuzzy Systems 40, no. 6 (2021): 11539–58. http://dx.doi.org/10.3233/jifs-202749.

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Commonality, a typical commercial feature of serialized civil aircraft study and development, refers to a series of methods of reusing and sharing assets, which were developed based on broad similarity. The common design of serialized civil aircraft is capable of maximally saving R&D, production, operation, and disposal. To maximize the total benefits of manufacturers and operators, the common design of serialized civil aircrafts primarily exploits the commercial experience of serialized products in other fields (e.g., automobiles and mobile phones), whereas a scientific index system and q

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14

Jackson, Scott, Mary J. Simpson, Cheryl Atkinson, et al. "8.6.1 Towards the Development of Domain‐Specific Guidelines for a Systems Engineering Framework: Commercial Aircraft." INCOSE International Symposium 10, no. 1 (2000): 831–38. http://dx.doi.org/10.1002/j.2334-5837.2000.tb00461.x.

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AbstractThe Joint Commercial Aircraft Working Group (JCAWG) consists of members from INCOSE, other professional societies, major aircraft manufacturers, regulatory agencies, suppliers, and other companies in the commercial aircraft domain. JCAWG is chairing the development of a supplemental guideline for the Commercial Aircraft Transport Domain under the title of “Guidelines for the Application of Systems Engineering in the Commercial Aircraft Domain.” The primary purpose of the Guidelines is to span the gap between the ANSI/EIA standard and other guidelines in the aircraft industry. These Gui

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15

Khan, Fatima Najeeb, Ayiei Ayiei, John Murray, Glenn Baxter, and Graham Wild. "A Preliminary Investigation of Maintenance Contributions to Commercial Air Transport Accidents." Aerospace 7, no. 9 (2020): 129. http://dx.doi.org/10.3390/aerospace7090129.

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Aircraft maintenance includes all the tasks needed to ensure an aircraft’s continuing airworthiness. Accidents that result from these maintenance activities can be used to assess safety. This research seeks to undertake a preliminary investigation of accidents that have maintenance contributions. An exploratory design was utilized, which commenced with a content analysis of the accidents with maintenance contributions (n = 35) in the official ICAO accident data set (N = 1277), followed by a quantitative ex-post facto study. Results showed that maintenance contributions are involved in 2.8 ± 0.

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16

Wang, X., H. Yu, and D. Feng. "Pose estimation in runway end safety area using geometry structure features." Aeronautical Journal 120, no. 1226 (2016): 675–91. http://dx.doi.org/10.1017/aer.2016.16.

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ABSTRACTA novel image-based method is presented in this paper to estimate the poses of commercial aircrafts in a runway end safety area. Based on the fact that similar poses of an aircraft will have similar geometry structures, this method first extracts features to describe the structure of an aircraft's fuselage and aerofoil by RANdom Sample Consensus algorithm (RANSAC), and then uses the central moments to obtain the aircrafts’ pose information. Based on the proposed pose information, a two-step feature matching strategy is further designed to identify an aircraft's particular pose. In orde

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17

Zhang, Ya Ni, Yan Li, and Ya Kui Gao. "Commercial Transport Aircraft Flight Simulator Flying Qualities Airworthiness Verification." Applied Mechanics and Materials 235 (November 2012): 170–75. http://dx.doi.org/10.4028/www.scientific.net/amm.235.170.

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Flight simulation is a simulation of flight and various aspects of the flight environment. Flight simulation is used for a variety of reasons, including aircraft development and flight training. The engineering flight simulator is used for a certain commercial transport aircraft development. The aircraft adopts fly-by-wire flight control technology. The engineering flight simulator was mainly used as a platform to test flying quality of the aircraft. The simulator has actual aircraft cockpit with wide-field visual system mounted on large six degree of freedom(DOF) motion platform that feature

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18

Gehlhoff, Felix, Hamied Nabizada, Maximilian Weigand, et al. "Challenges in Automated Commercial Aircraft Production." IFAC-PapersOnLine 55, no. 2 (2022): 354–59. http://dx.doi.org/10.1016/j.ifacol.2022.04.219.

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19

Chalk, Andrew J. "Market Forces and Commercial Aircraft Safety." Journal of Industrial Economics 36, no. 1 (1987): 61. http://dx.doi.org/10.2307/2098597.

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20

Ross, Tamaira E., and William A. Crossley. "Method to Assess Commercial Aircraft Technologies." Journal of Aircraft 37, no. 4 (2000): 570–79. http://dx.doi.org/10.2514/2.2668.

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21

Zyweck, A., and R. E. Bogner. "Radar target classification of commercial aircraft." IEEE Transactions on Aerospace and Electronic Systems 32, no. 2 (1996): 598–606. http://dx.doi.org/10.1109/7.489504.

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22

Moninger, William R., Richard D. Mamrosh, and Patricia M. Pauley. "Automated Meteorological Reports from Commercial Aircraft." Bulletin of the American Meteorological Society 84, no. 2 (2003): 203–16. http://dx.doi.org/10.1175/bams-84-2-203.

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23

Gavrilović, Nikola N., Boško P. Rašuo, George S. Dulikravich, and Vladimir B. Parezanović. "Commercial aircraft performance improvement using winglets." FME Transaction 43, no. 1 (2015): 1–8. http://dx.doi.org/10.5937/fmet1501001g.

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24

Gao, N. P., and J. L. Niu. "Personalized Ventilation for Commercial Aircraft Cabins." Journal of Aircraft 45, no. 2 (2008): 508–12. http://dx.doi.org/10.2514/1.30272.

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25

Bewlay, B. P., S. Nag, A. Suzuki, and M. J. Weimer. "TiAl alloys in commercial aircraft engines." Materials at High Temperatures 33, no. 4-5 (2016): 549–59. http://dx.doi.org/10.1080/09603409.2016.1183068.

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26

Christenson, D. W. "Interfacing aircraft to commercial personal computers." IEEE Aerospace and Electronic Systems Magazine 16, no. 5 (2001): 11–16. http://dx.doi.org/10.1109/62.925691.

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27

Eatough, Delbert J., Fern M. Caka, John Crawford, Scott Braithwaite, Lee D. Hansen, and Edwin A. Lewis. "Environmental tobacco smoke in commercial aircraft." Atmospheric Environment. Part A. General Topics 26, no. 12 (1992): 2211–18. http://dx.doi.org/10.1016/0960-1686(92)90410-m.

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28

McLean, Donald. "Operational Efficiency of Commercial Transport Aircraft." Measurement and Control 38, no. 8 (2005): 243–48. http://dx.doi.org/10.1177/002029400503800803.

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29

Baldeschwieler, John D. "Explosive detection for commercial aircraft security." Terrorism and Political Violence 5, no. 2 (1993): 81–102. http://dx.doi.org/10.1080/09546559308427209.

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30

WANG, Tongan, and Norbert ANTESBERGER. "Large commercial business aircraft acoustic design with SEA." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 270, no. 8 (2024): 3115–20. http://dx.doi.org/10.3397/in_2024_3276.

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As air travel becomes more frequent, customers are demanding a quieter cabin environment. Over the past two decades, Gulfstream has developed a suite of predictive tools based on Statistical Energy Analysis (SEA) to create a quiet cabin on business aircraft. This paper discusses the most recent collaboration between Gulfstream and Jet Aviation to develop an acoustic design for a large commercial business aircraft. SEA analysis played a key role to identify the risks, determine the driving mechanisms, and develop solutions to meet the established target. Besides SEA model development and analys

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31

Hartjes, Sander, Hendrikus G. Visser, and Marco E. G. van Hellenberg Hubar. "Trajectory Optimization of Extended Formation Flights for Commercial Aviation." Aerospace 6, no. 9 (2019): 100. http://dx.doi.org/10.3390/aerospace6090100.

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This paper presents a trajectory optimization study that has been conducted using a recently developed tool for the synthesis and analysis of extended flight formations of long-haul commercial aircraft, with the aim to minimize overall fuel consumption. In extended flight formations, trailing aircraft can attain an appreciable reduction in induced drag and associated reduction in fuel burn by flying in the upwash of the lead aircraft’s wake. In the present study, a previously developed multi-phase optimal control (MOC) framework for the synthesis of two-ship flight formations has been extended

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32

Vuorinen, Mari, Pentti Varpasuo, and Jukka Kahkonen. "ICONE19-43207 Reaction-time response of a large commercial aircraft." Proceedings of the International Conference on Nuclear Engineering (ICONE) 2011.19 (2011): _ICONE1943. http://dx.doi.org/10.1299/jsmeicone.2011.19._icone1943_81.

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33

Sarlioglu, Bulent, and Casey T. Morris. "More Electric Aircraft: Review, Challenges, and Opportunities for Commercial Transport Aircraft." IEEE Transactions on Transportation Electrification 1, no. 1 (2015): 54–64. http://dx.doi.org/10.1109/tte.2015.2426499.

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34

Drüe, C., W. Frey, A. Hoff, and Th Hauf. "Aircraft type-specific errors in AMDAR weather reports from commercial aircraft." Quarterly Journal of the Royal Meteorological Society 134, no. 630 (2008): 229–39. http://dx.doi.org/10.1002/qj.205.

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35

Rivas, Damián, Alfonso Valenzuela, and José L. de Augusto. "Computation of global trajectories of commercial transport aircraft." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 227, no. 1 (2012): 142–58. http://dx.doi.org/10.1177/0954410011427107.

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A trajectory computation tool designed to compute global trajectories (from take off to landing) of commercial transport aircraft is presented. The global trajectory is defined by a general flight intent, considering flight segments usually flown by transport aircraft, including standard airline procedures, and air traffic control regulations. The computation is based on a trajectory computation solver designed for a general aircraft performance model (general drag polar and general engine model); the formulation takes into account wind effects and temperature corrections for a non-standard at

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36

Xu, Haizhao, and Lijun Yang. "Research on modular design requirements of commercial aircraft." Journal of Physics: Conference Series 2955, no. 1 (2025): 012018. https://doi.org/10.1088/1742-6596/2955/1/012018.

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Abstract It is urgent to have a unified design process and methodology for modular manufacturing during the initial stage of a civil commercial aircraft project because it involves diverse stakeholders and covers almost the entire commercial aircraft industry chain. This paper presents a Need-Function-Requirement-Physics (N-F-R-P) based system engineering forward design model to determine the set of modular design processes and criteria for the project. Based on the investigation of the stakeholders of the commercial aircraft design, the proposed model first forms the requirement list of modul

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37

Malyshev, Viktor, Angelina Gab, Viktoriia Kovalenko, Yurii Lipskyi, and Dmytro Shakhnin. "Estimation of the world market and application of nanomaterials in the aerospace industry." Technology audit and production reserves 5, no. 4(79) (2024): 29–41. http://dx.doi.org/10.15587/2706-5448.2024.312875.

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The object of the study is the global aerospace market status, segment analysis, dynamics, competition, and prospects. The methods of searching and analyzing literature data, summarizing, systematizing, and visualizing data with diagrams are used. The aerospace industry is at the forefront of technological innovation and is constantly searching for new advanced materials to improve productivity, efficiency, and safety. The aerospace market encompassing the design, manufacture, and maintenance of aircrafts, space vehicles, and related systems. It includes the commercial and military sectors, as

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38

Tom, Liya, Muhammad Khowja, Gaurang Vakil, and Chris Gerada. "Commercial Aircraft Electrification—Current State and Future Scope." Energies 14, no. 24 (2021): 8381. http://dx.doi.org/10.3390/en14248381.

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Electric and hybrid-electric aircraft propulsion are rapidly revolutionising mobility technologies. Air travel has become a major focus point with respect to reducing greenhouse gas emissions. The electrification of aircraft components can bring several benefits such as reduced mass, environmental impact, fuel consumption, increased reliability and quicker failure resolution. Propulsion, actuation and power generation are the three key areas of focus in more electric aircraft technologies, due to the increasing demand for power-dense, efficient and fault-tolerant flight components. The necessi

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39

Vladimirov, Y. "PROGRESS BEYOND THE CLOUDS AND METAMORPHOSIS OF TIME." World of Transport and Transportation 16, no. 5 (2018): 272–76. http://dx.doi.org/10.30932/1992-3252-2018-16-5-18.

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For the English full text of the article please see the attached PDF-File (English version follows Russian version).Sobolev, Dmitry A. The history of development of passenger aircrafts (1910-1970s): To the 100th anniversary of civil aviation. Moscow, «Russkie Vityazi» Foundation, 2018, 264 p. ABSTRACT The book is devoted to the history of development of passenger aircrafts from the beginning of their appearance until the mid-1970s. The book tells how the first passenger aircrafts appeared and civil aviation became more and more in demand, which was intended to master the previously inaccessibl

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40

Lü, Zhi, Zhan Gao, and Yi Lü. "A Flight Simulator that Grouping Aircrafts Simultaneously Take off and Land in Open Grid Computing Environment." Applied Mechanics and Materials 182-183 (June 2012): 1292–97. http://dx.doi.org/10.4028/www.scientific.net/amm.182-183.1292.

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The performance of airplane in commercial airline environment is determined by, and therefore an indicator of performance measure of, the thermodynamic properties of airplane. The aim of this study was to establish the use of simulators to determine aircraft accident for a flight of airplanes and evaluate the potential of new airspace structure and airport’s runway. This indicates that there is a possibility of obtaining airplane performance from analysis and verification simulating airplane. As compared with AIRBUS Full Flight Simulator, a multiple aircrafts flight simulator that grouping air

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41

Tirovolis, N. L., and V. C. Serghides. "A methodology for the assessment of unit cost drivers for commercial aircraft." Aeronautical Journal 110, no. 1105 (2006): 173–84. http://dx.doi.org/10.1017/s0001924000001159.

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Abstract Presented in this paper are the prerequisite steps in a methodology for the identification and assessment of unit cost drivers for use in the development of a new design-oriented unit cost estimation methodology for large commercial jet aircraft with minimum seating capacity of 100 passengers. The work presented here focuses on unit cost, which is a significant element of the total aircraft cost and for the initial aircraft design process in particular. The methodology aims to investigate how aircraft design properties could influence cost. Cost estimation relationships, containing a

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42

Giuliani, Michelangelo, Ignazio Dimino, Salvatore Ameduri, Rosario Pecora, and Antonio Concilio. "Status and Perspectives of Commercial Aircraft Morphing." Biomimetics 7, no. 1 (2022): 11. http://dx.doi.org/10.3390/biomimetics7010011.

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In a previous paper, the authors dealt with the current showstoppers that inhibit commercial applicability of morphing systems. In this work, the authors express a critical vision of the current status of the proposed architectures and the needs that should be accomplished to make them viable for installation onboard of commercial aircraft. The distinction is essential because military and civil issues and necessities are very different, and both the solutions and difficulties to be overcome are widely diverse. Yet, still remaining in the civil segment, there can be other differences, dependin

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43

Tirovolis, Nikolaos L., and Varnavas C. Serghides. "Unit Cost Estimation Methodology for Commercial Aircraft." Journal of Aircraft 42, no. 6 (2005): 1377–86. http://dx.doi.org/10.2514/1.12491.

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44

Turiak, Marek, Alena Novák Sedláčková, and Andrej Novák. "Flight Recorders - Alternative Concept for Commercial Aircraft." MAD - Magazine of Aviation Development 3, no. 16 (2015): 32–36. http://dx.doi.org/10.14311/mad.2015.16.08.

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This paper deals with the issue of deployable flight data recorders. It gives an insight into pros and cons of this solution based on experience gained in military application. Advantages of such solution are at least worth considering as they may help reduce the number of accidents and save lives in the first place. And should the accident happen the location and extraction of evidence is much easier.

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45

Qi, Pan Guo, D. C. Cong, H. J. Jiang, and Jun Wei Han. "Systems Analysis for Commercial Aircraft Flight Simulator." Applied Mechanics and Materials 10-12 (December 2007): 522–27. http://dx.doi.org/10.4028/www.scientific.net/amm.10-12.522.

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Flight simulator is a complex man-in-the-loop (MIL) simulation system. With several decades of development, it has already become important tools of aircraft design and development, and necessary means of pilot training. And simulation credibility and reliability of the flight simulator have been considerably improved in comparison with the past. However, the system of flight simulator has become increasingly complex and difficult to be described clearly. This paper presents the concepts of conceptual layer and achieving layer, analyzes the composition and principle of the commercial aircraft

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46

Voge, Victoria, and Lance Schaeffer. "POTENTIAL RAINBOE TOXICITY IN COMMERCIAL AIRCRAFT COCKPITS." Southern Medical Journal 89, Supplement (1996): S70. http://dx.doi.org/10.1097/00007611-199610001-00133.

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47

Schennetten, Kai, Matthias M. Meier, and Markus Scheibinger. "Measurement of UV radiation in commercial aircraft." Journal of Radiological Protection 39, no. 1 (2018): 85–96. http://dx.doi.org/10.1088/1361-6498/aaf2a7.

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48

Herndon, Scott C., Timothy B. Onasch, Brian P. Frank, et al. "Particulate Emissions from in-use Commercial Aircraft." Aerosol Science and Technology 39, no. 8 (2005): 799–809. http://dx.doi.org/10.1080/02786820500247363.

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49

Carbaugh, Robert J. "Strategic trade policy and commercial jet aircraft." International Trade Journal 7, no. 4 (1993): 393–408. http://dx.doi.org/10.1080/08853909308523772.

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50

Tompa, Rachael E., and Mykel J. Kochenderfer. "Efficient Aircraft Rerouting During Commercial Space Launches." New Space 7, no. 1 (2019): 12–18. http://dx.doi.org/10.1089/space.2018.0032.

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