Relevant bibliographies by topics / Runways (Aeronautics) Mathematical models

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Runways (Aeronautics) Mathematical models'

Author: Grafiati
Published: 10 December 2022
Last updated: 31 July 2025

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Journal articles on the topic "Runways (Aeronautics) Mathematical models"

1

Cao, Yihua, Yong Chen, and Yong Zhou. "Studies of capacity estimation of the airport with two parallel runways." Aeronautical Journal 109, no. 1098 (2005): 395–401. http://dx.doi.org/10.1017/s0001924000000816.

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Abstract The analytical capacity models of an airport with two runways system are developed in this paper and the theoretical capacity curves yielded by this model are analysed. The statistic airport capacity estimation methodology based on historical data is introduced as well. Both analytical models and statistic strategy are applied to estimate the capacity of the two runways system of a typical airport. Two sets of airport capacity curves obtained in different ways are compared and analysed. The result of the analysis indicates that the mathematical model works effectively in a fairly accu
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Ilie, Constantin Ovidiu, Dănuț Grosu, Oana Mocian, Radu Vilău, and Daniela Bartiș. "Using Statistically Based Modeling for Vehicle Dynamics." Advanced Materials Research 1036 (October 2014): 564–67. http://dx.doi.org/10.4028/www.scientific.net/amr.1036.564.

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This paper is a result of a research focused on statistical vehicles dynamics. Its main purpose is to establish mathematical description of vehicle dynamics based on statistically sufficient experimental data and using statistical instruments. The results are analytical expressions and graphical representations that can be used in situations other than those the data were obtained. Experimental research program objective was to obtain a variety of data to define the dynamics of a vehicle. It involved a large number of tests, more than 100, on different runways, pavement, mosaic tiles or asphal
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Chen, Haotian, Yijun Liu, and Yunuo Zhang. "Research on the Aerodynamic Performance of an Airfoil." Journal of Physics: Conference Series 2469, no. 1 (2023): 012029. http://dx.doi.org/10.1088/1742-6596/2469/1/012029.

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Abstract Airfoils provide lift force for planes and keep planes flying in the atmosphere. Different airfoils have distinct performance characteristics based on their shapes, influencing the flying condition of planes and people’s safety. Therefore, an airfoil’s shape must be carefully studied and deliberated on because it’s an engineer’s professional duty to protect people’s safety with engineering knowledge. In this paper, physical and mathematical models are applied to analyze the shape and corresponding characteristics of an airfoil. Models, including Bernoulli’s Equation and Ideal gas Law,
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Li, Daijin, and Kai Luo. "One-Dimensional Model Incorporated with Mechanical Loss and Auxiliary Power for Evaluating Thermodynamic Performance of Stirling Engine." International Journal of Nonlinear Sciences and Numerical Simulation 17, no. 3-4 (2016): 137–48. http://dx.doi.org/10.1515/ijnsns-2014-0063.

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AbstractStirling engines are regarded as an efficient and promising power system for underwater devices. Currently, many models have been used to evaluate thermodynamic performance of Stirling engine, but in which mechanical loss and auxiliary power still cannot be modeled with proper mathematical models. A four-cylinder double-acting Stirling engine for Unmanned Underwater Vehicle (UUV) is discussed in this paper. Referring to the Stirling engine experimental results from National Aeronautics and Space Administration (NASA), a one-dimensional model incorporated with empirical equations of mec
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Kretulis, V. S. "INVESTIGATION OF THE INFLUENCE OF CORRELATED COLOR TEMPERATURE OF LED illuminatorS AS A FACTOR OF SAFETY LIGHTING OF HIGHWAYS FOR DIFFICULT WEATHER CONDITIONS." Optoelektronìka ta napìvprovìdnikova tehnìka 56 (December 7, 2021): 89–96. http://dx.doi.org/10.15407/iopt.2021.56.089.

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A investigation of the dependence of relative horizontal illumination level and brightness of the most common types of road surface in Ukraine when using LED illuminators with different spectral distribution of radiation in the presence of aerial aerosols of different optical densities (strong, moderate, weak fog and haze) is performed. Mathematical models of LED illuminators with correlated color temperature Tcc = (2200÷8400) K in the visible range of the spectrum λ = (380÷780) nm have been created. Their use together with the selected model of the spectral dependence of the scattering index
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Nzao, Anthony Bassesuka Sandoka. "Study of the Simulation and Application of the PEEC Method for Modeling the Prediction of Emissions Radiated by the Onboard Electronic Wiring System." Computer and Information Science 17, no. 2 (2024): 7. http://dx.doi.org/10.5539/cis.v17n2p7.

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The coexistence of electronic power and control systems in the same box presents a serious threat to the proper functioning of electronic systems integrated into automobiles, aeronautics and space. Thus, managing the electromagnetic compatibility of these systems constitutes a challenge, particularly given electromagnetic phenomena. This paper describes a simulation study and application of the partial element equivalent circuit method to model the prediction of radiated emissions from the onboard electronic cable system. In this article, we first explain the use of the partial cell equivalent
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Vyshinsky, V. V., та K. T. Zoan. "Аtmospheric wind flow around the mountain landscape in the vicinity of Danang airport and flight safety issues". Civil Aviation High Technologies 24, № 6 (2021): 27–41. http://dx.doi.org/10.26467/2079-0619-2021-24-6-27-41.

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Wind boundary layer flow over the mountain landscape and large structures located around runways (RWs) creates coherent vortex structures (CVSs) that can cross a glideslope and airspace in the vicinity of an airport. The aircraft, encountering a vortex structure, experiences significant changes of the aerodynamic forces and moments, what is especially hazardous due to proximity to terrain. From a mathematical point of view, the solution of this problem presents a challenge due to extremely large space – time scale of the phenomenon, the lack of relevant atmospheric models, as well as comprehen
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Ketabdari, Misagh, Ignacio P. Millán, Emanuele Toraldo, Maurizio Crispino, and Mariano Pernetti. "Analytical Optimization Model to Locate and Design Runway-Taxiway Junctions." Open Civil Engineering Journal 15, no. 1 (2021): 347–59. http://dx.doi.org/10.2174/1874149502115010347.

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Aims: Air traffic and airport operations are expected to experience significant growth worldwide in the upcoming years. One of the possible approaches to adapt to this demand-led growth in the sector, while guaranteeing optimal levels of airport services and operations safety, is to maximize the capacities of busy airport infrastructures (in particular runways) by evacuating them in the shortest time possible to be ready for hosting next operations. Background: The main research areas in this field range from statistical risk analyses based on the registered accidents databases to simulation a
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De Lemos, Hugo, Michel M. Verstraete, and Mary Scholes. "Parametric Models to Characterize the Phenology of the Lowveld Savanna at Skukuza, South Africa." Remote Sensing 12, no. 23 (2020): 3927. http://dx.doi.org/10.3390/rs12233927.

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Mathematical models, such as the logistic curve, have been extensively used to model the temporal evolution of biological processes, though other similarly shaped functions could be (and sometimes have been) used for this purpose. Most previous studies focused on agricultural regions in the Northern Hemisphere and were based on the Normalized Difference Vegetation Index (NDVI). This paper compares the capacity of four parametric double S-shaped models (Gaussian, Hyperbolic Tangent, Logistic, and Sine) to represent the seasonal phenology of an unmanaged, protected savanna biome in South Africa’
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Soelem, Aafnan Bhuiyan. "Formulation of Flood Inundation Map in Jamalpur District by Mathematical Modeling using HEC Packages." Journal of Water Resources and Pollution Studies 3, no. 3 (2018): 33–66. https://doi.org/10.5281/zenodo.1560739.

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Bangladesh lies in the convergence zone of three large rivers of the world-Ganges, Brahmaputra, Meghna, which is called the GBM basin. The Ganges, Brahmaputra and Meghna (GBM) river basins occupy about 1.75 x 106 km<sup>2</sup> of the Himalayan region. More than half a billion people in Nepal, India, Bhutan and Bangladesh are directly or indirectly dependent on the water resources of the GBM rivers. Being in this zone, Bangladesh faces heavy rainfall in the monsoon season of June to October, thus a huge amount of water drains out each year through the country. This drain out, along with variou
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Dissertations / Theses on the topic "Runways (Aeronautics) Mathematical models"

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Kim, Byung Jong. "Optimal runway exit design and capacity enhancement." Diss., Virginia Tech, 1993. http://hdl.handle.net/10919/38637.

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Congestion and delay problems at airports have received much attention in recent years because of the unbalanced condition between demand and supply. Recent demand forecasts indicate that the problems are expected to increase in the next decade. Relieving congestion of the air transportation networks requires several strategies to enhance the runway capacity. Among these strategies is reducing the runway occupancy time a critical factor in affecting runway capacity. And one approach to reducing the runway occupancy time (ROT) is locating the high speed exits optimally. In addressing the reduc
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Knight, Peter Robin. "Artificial intelligence and mathematical models for intelligent management of aircraft data." Thesis, University of Southampton, 2012. https://eprints.soton.ac.uk/355717/.

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Increasingly, large volumes of aircraft data are being recorded in an effort to adapt aircraft maintenance procedures from being time-based towards condition-based techniques. This study uses techniques of artificial intelligence and develops mathematical models to analyse this data to enable improvements to be made in aircraft management, affordability, availability, airworthiness and performance. In addition, it highlights the need to assess the integrity of data before further analysis and presents the benefits of fusing all relevant data sources together. The research effort consists of th
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Kumar, Niraj. "A genetic algorithm based approach for air cargo loading problem." Thesis, Click to view the E-thesis via HKUTO, 2006. http://sunzi.lib.hku.hk/hkuto/record/B38576818.

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Yao, Yufeng. "Topics in Fractional Airlines." Diss., Georgia Institute of Technology, 2007. http://hdl.handle.net/1853/14563.

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Fractional aircraft ownership programs offer companies and individuals all the benefits of owning private jet, such as safety, consistency, and guaranteed availability, at a fraction of the cost of owning an aircraft. In the fractional ownership model, the partial owners of an aircraft are entitled to certain number of hours per year, and the management company is responsible for all the operational considerations and making sure an aircraft is available to the owners at the requested time and location. This thesis research proposes advance optimization techniques to help the management compa
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Baig, Saood Saeed. "A simple moving boundary technique and its application to supersonic inlet starting /." Thesis, McGill University, 2008. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=112555.

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In this thesis, a simple moving boundary technique has been suggested, implemented and verified. The technique may be considered as a generalization of the well-known "ghost" cell approach for boundary condition implementation. According to the proposed idea, the moving body does not appear on the computational grid and is allowed to move over the grid. The impermeable wall boundary condition is enforced by assigning proper gasdynamic values at the grid nodes located inside the moving body close to its boundaries (ghost nodes). The reflection principle taking into account the velocity of the b
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Zhao, Yiming. "Efficient and robust aircraft landing trajectory optimization." Diss., Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/43586.

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This thesis addresses the challenges in the efficient and robust generation and optimization of three-dimensional landing trajectories for fixed-wing aircraft subject to prescribed boundary conditions and constraints on maneuverability and collision avoidance. In particular, this thesis focuses on the airliner emergency landing scenario and the minimization of landing time. The main contribution of the thesis is two-fold. First, it provides a hierarchical scheme for integrating the complementary strength of a variety of methods in path planning and trajectory optimization for the improvement i
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"Growth, competitions and strategies in the air transport industry in Pearl River Delta of China." 2008. http://library.cuhk.edu.hk/record=b5893637.

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Xu, Fang.<br>Thesis (M.Phil.)--Chinese University of Hong Kong, 2008.<br>Includes bibliographical references (leaves 75-79).<br>Abstracts in English and Chinese.<br>Abstract --- p.i<br>Acknowledgement --- p.ii<br>Chapter 1 --- Introduction --- p.1<br>Chapter 2 --- Background Information --- p.3<br>Chapter 2.1 --- Growth of Air-Transportation Industry --- p.3<br>Chapter 2.1.1 --- General Figures --- p.3<br>Chapter 2.1.2 --- Growth of Air Cargo Market --- p.3<br>Chapter 2.1.3 --- Regulatory Support --- p.5<br>Chapter 2.2 --- The Focus: Pearl River Delta --- p.6<br>Chapter 2.2.1 --- Stra
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"Monitoring air cargo shipments: a framework for detecting potential delays and prescribing corrective measures." 2007. http://library.cuhk.edu.hk/record=b5893196.

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Wan, Yulai.<br>Thesis (M.Phil.)--Chinese University of Hong Kong, 2007.<br>Includes bibliographical references (leaves 42-44).<br>Abstracts in English and Chinese.<br>Abstract --- p.i<br>Acknowledgement --- p.iii<br>Chapter Chapter 1 --- Introduction --- p.1<br>Chapter Chapter 2 --- Literature Review --- p.6<br>Chapter Chapter 3 --- Framework --- p.10<br>Chapter Chapter 4 --- The Simulation Model --- p.13<br>Chapter Chapter 5 --- Phase 1: Detect Potential Delay --- p.15<br>Chapter 5.1 --- The delay indicator --- p.15<br>Chapter 5.2 --- Setting tolerance level --- p.20<br>Chapter Chapt
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Weldon, John Phillips. "Dimensioned system dynamics modeling with external subprograms for Air Force aviation fuel." Phd thesis, 1993. http://hdl.handle.net/1885/145688.

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Turner, Sheelah Anne. "An application of a gravity model to air cargo at Vancouver International Airport." Thesis, 2002. http://hdl.handle.net/2429/12234.

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There has been very little research in the area of air cargo demand analysis and forecasting. This thesis attempts to investigate the application of gravity models to air cargo. Using international export volumes from Vancouver International Airport in 1998, a gravity model was built. The inclusion of tariffs as an impedance factor allowed testing of the effect of tariffs as predicted by gravity models. The results were consistent with international trade theory that tariffs provide a barrier to international trade. Further, a comparison is made between aggregate and disaggregate models
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Books on the topic "Runways (Aeronautics) Mathematical models"

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Szydło, Antoni. Statyczna identyfikacja parametrów modeli nawierzchni lotniskowych. Oficyna Wydawnicza Politechniki Wrocławskiej, 1995.

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Samanant, Paul. Description of the AILS alerting algorithm. National Aeronautics and Space Administration, Langley Research Center, 2000.

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Waller, Marvin C. An analysis of the role of ATC in the AILS concept. National Aeronautics and Space Administration, Langley Research Center, 2000.

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National Research Council (U.S.). Transportation Research Board., ed. Modeling and analysis of airport and aircraft operations. Transportation Research Board, 1989.

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G, Totiashvili L., and Rīgas civīlās aviācijas inženieru institūts., eds. Matematicheskoe modelirovanie zadach dinamiki i bezopasnosti poletov v grazhdanskoĭ aviat͡s︡ii: Sbornik nauchnykh trudov. RIO RKIIGA, 1987.

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Zhivetin, Vladimir. Metody i sredstva obespechenii︠a︡ bezopasnosti poleta: Riski i bezopasnostʹ aviat︠s︡ionnykh sistem. In-t problem riska, 2010.

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G, T͡S︡ipenko V., and Moskovskiĭ institut inzhenerov grazhdanskoĭ aviat͡s︡ii., eds. Matematicheskoe modelirovanie v zadachakh letnoĭ ėkspluatat͡s︡ii vozdushnykh sudov: Sbornik nauchnykh trudov. Moskovskiĭ in-t inzhenerov grazhdanskoĭ aviat͡s︡ii, 1993.

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Center, Langley Research, ed. Numerical simulation of swept-wing flows: A progress report for graduate program in aeronautics. National Aeronautics and Space Administration, Langley Research Center, 1991.

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M, Adelman Howard, Haftka Raphael T, United States. National Aeronautics and Space Administration., and Virginia Polytechnic Institute and State University., eds. Sensitivity analysis in engineering: Proceedings of a symposium sponsored by the National Aeronautics and Space Administration and Virginia Polytechnic Institute and State University, and held at Langley Research Center, Hampton, Virginia, September 25-26, 1986. NASA, Scientific and Technical Information Branch, 1987.

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Ozoka, Angus Ifeanyi. Aviation facilities planning, research, and development: A global experience. Nigerian Gong Press, 1997.

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Book chapters on the topic "Runways (Aeronautics) Mathematical models"

1

Feistauer, M., J. Felcman, and I. Straskraba. "Finite Difference and Finite Volume Methods for Nonlinear Hyperbolic Systems and the Euler Equations." In Mathematical and Computational Methods for Compressible Flow. Oxford University PressOxford, 2003. http://dx.doi.org/10.1093/oso/9780198505884.003.0004.

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Abstract In modern technologies one often encounters the necessity to solve compressible flow with a complicated structure. There are several conceivable models of compressible flow. Let us mention, for example, the model of inviscid, stationary, irrotational or rotational subsonic flow using the stream function formulation, and the models of transonic flow based on the small perturbation equation or full potential equation. There exists an extensive literature about the finite difference or finite element methods for the numerical solution of these models. (For a survey of mathematical and nu
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Oukassi, Abdellah. "Implementing ADRC and PI Controls for a Sensorless Induction Motor Supplied by a Multi-Level Converter and Using PV Sources." In Induction Motors - Latest Research and Applications. IntechOpen, 2025. https://doi.org/10.5772/intechopen.1006027.

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The proposed book will focus on the controls of induction machines aimed at exploiting them in the field of speed variation (electric vehicles, aeronautics, etc.). In this work, the authors utilize cascaded multi-level converters to reduce the harmonic distortion rate of the voltages at the machine’s input. The converter is controlled by pulse width modulation (PWM) technique. The use of active disturbance rejection control (ADRC) will contribute to eliminating internal disturbances (undesired variations in machine resistances) as well as minimizing external effects (inertia, resisting torque)
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Conference papers on the topic "Runways (Aeronautics) Mathematical models"

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Pawlus, W., J. E. Nielsen, H. R. Karimi, and K. G. Robbersmyr. "Further results on mathematical models of vehicle localized impact." In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (ISSCAA 2010). IEEE, 2010. http://dx.doi.org/10.1109/isscaa.2010.5634041.

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Fonzi, N. "New insights on limit cycle oscillations due to control surface freeplay." In Aeronautics and Astronautics. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902813-9.

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Abstract. A new experimental wind tunnel test-bed has been developed for the study of limit cycle oscillations induced by control surface freeplay. Studies of the effects of a single nonlinearity, made possible by the new horizontal tail plane, are described here. Several effects are considered, starting from a reference configuration: the effect of changes in inertia and stiffness, a time-varying gap size, and an aerodynamic preload due to an angle of attack. Both time marching simulations and describing functions analytical methods have been used to understand the experimental measurements a
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Maroufkhani, Aida, Claire Charpentier, Francois Morency, and Gelareh Momen. "Effect of Variable Melting Temperature on the Enthalpy Model for Runway Deicing." In International Conference on Icing of Aircraft, Engines, and Structures. SAE International, 2023. http://dx.doi.org/10.4271/2023-01-1441.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;One of the most significant challenges for the aviation industry in the winter is the deicing operations on runways. As a result, deicer chemicals can pollute the environment if used in a large amount. A mathematical model could help optimize the use of deicer chemicals. Road deicing models exist to predict pavement temperature covered by snow/ice during deicing operations. However, the specificity of airport operations requires a model for the runway deicing to simulate the mass of ice melted with usage of deicing agent
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