Gotowe bibliografie tematyczne / Aerodynamics

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Gotowa bibliografia na temat „Aerodynamics”

Autor: Grafiati

Data publikacji: 4 czerwca 2021

Data aktualizacji: 29 lipca 2024

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Artykuły w czasopismach na temat "Aerodynamics"

Ološtiak, Martin. "To the relations between morphemic and word-formation structure of a word in Slovak". Journal of Linguistics/Jazykovedný casopis 70, nr 3 (1.12.2019): 545–72. http://dx.doi.org/10.2478/jazcas-2020-0004.

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AbstractThe paper focuses on relations between word-formation and morphemic structure of a Slovak word based on the material from Slovník koreňových morfém slovenčiny [Slovak Dictionary of Root Morphemes] (Sokolová et al., 2012). Particularly, manifestations of morphemic variation determined by word-formation poly-motivation are analysed. Poly-motivation arises from the re-grouping of the relations within a word-formation nest, where the mediated motivation can be understood as an alternative direct motivation, e.g. aerodynamika [noun, ‘aerodynamics’] → (aerodynamický [adjective, ‘related to aerodynamics’]) → aerodynamicky [adverb]. The adverb aerodynamicky is derived from the adjective (aerodynamický → aerodynamick-y ‘in an aerodynamic manner’) as well as from the noun (aerodynamika → aerodynamic-ky ‘with regard to aerodynamics’). Thus, the structure of affixes can be extended as a result of infixation conditioned by poly-motivation, cf. aerodynamick-y (suffix -y) / aerodynamic-ky (suffix -y with an infix: -k:y). As far as poly-motivation is concerned, a particular affix can have several morphemic and word-formation manifestations, e.g. Slovak adverb suffix -y can be manifested as -y, -ky, -icky, -isticky, -sky, -euticky, -aticky, -eticky, -ecky, -nícky.

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Tian, Hong-qi. "Review of research on high-speed railway aerodynamics in China". Transportation Safety and Environment 1, nr 1 (1.07.2019): 1–21. http://dx.doi.org/10.1093/tse/tdz014.

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Abstract High-speed railway aerodynamics is the key basic science for solving the bottleneck problem of high-speed railway development. This paper systematically summarizes the aerodynamic research relating to China’s high-speed railway network. Seven key research advances are comprehensively discussed, including train aerodynamic drag-reduction technology, train aerodynamic noise-reduction technology, train ventilation technology, train crossing aerodynamics, train/tunnel aerodynamics, train/climate environment aerodynamics, and train/human body aerodynamics. Seven types of railway aerodynamic test platform built by Central South University are introduced. Five major systems for a high-speed railway network—the aerodynamics theoretical system, the aerodynamic shape (train, tunnel, and so on) design system, the aerodynamics evaluation system, the 3D protection system for operational safety of the high-speed railway network, and the high-speed railway aerodynamic test/computation/analysis platform system—are also introduced. Finally, eight future development directions for the field of railway aerodynamics are proposed. For over 30 years, railway aerodynamics has been an important supporting element in the development of China’s high-speed railway network, which has also promoted the development of high-speed railway aerodynamics throughout the world.

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Philpot, M. G. "Future challenges for powerplant aerodynamic integration in combat aircraft". Aeronautical Journal 105, nr 1048 (czerwiec 2001): 335–43. http://dx.doi.org/10.1017/s0001924000012227.

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Abstract The operational requirements of modern combat aircraft demand complex engine intake and exhaust systems, capable of working efficiently over a very wide range of flight conditions and throttle settings. In addition to high aerodynamic efficiency and avoidance of high distortion levels at the engine face, these systems must also meet rigorous radar and infra-red signature targets. This paper discusses the implications from the aerodynamics point of view. Examples of technical approaches which seek to balance the sometimes conflicting requirements of aerodynamics and signatures are outlined. The potential offered by in-flight thrust vectoring to enhance flight performance and/or safety is also reviewed and the aerodynamic implications considered. Overall, propulsion integration for combat aircraft presents several challenges to the aerodynamicist, not least the development and validation of improved theoretical design methods capable of analysing the highly complex flows involved.

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Ji, Rui, Yinting Shen i Kai Sheng. "The recent progress and state-of-art applications of aerodynamics for vehicle". Highlights in Science, Engineering and Technology 13 (21.08.2022): 75–81. http://dx.doi.org/10.54097/hset.v13i.1334.

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Transportation is an indispensable part of human beings’ daily life, thus plenty of scholars have focused on improving the energy efficiency of transportation. The application and development of aerodynamics is of paramount importance. In this article, the effects of three types of locomotives on aerodynamic performance of high-speed trains are investigated. In order to lucubrate this topic, the definition of aerodynamics by different scientists is firstly discussed and showed, they basically classify them by three different kinds of ways. Subsequently, the creation of aerodynamics, historical development, and present situation are briefly introduced. In the main part, mathematical model and calculation formula are carried out to ensure which kinds of aerodynamic model is the most suitable among all the designs. Overall, these results offer a guideline for how to design a more effective and practical train head by applying the aerodynamic knowledge and expanding people's use of aerodynamics.

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Hong, Sungchan, Takeshi Asai i Byung Mook Weon. "Surface Patterns for Drag Modification in Volleyballs". Applied Sciences 9, nr 19 (25.09.2019): 4007. http://dx.doi.org/10.3390/app9194007.

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Surface patterns on objects are important in aerodynamics. We show how surface patterns on volleyballs modify their aerodynamic performances. Conventional volleyballs with six panels show different aerodynamic characteristics along transverse and diagonal directions. Interestingly, isotropic surface patterning with hexagons or dimples enables us to achieve isotropic aerodynamics. This result gives insight into surface-mediated flight controls of projectiles through resisting fluid media.

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Bielek, Boris, Daniel Szabó, Josip Klem i Kristína Kaniková. "Application of physical theory of cavity in the construction of double skin facades". Curved and Layered Structures 9, nr 1 (3.11.2021): 40–53. http://dx.doi.org/10.1515/cls-2022-0004.

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Abstract The article deals with the issue of double skin transparent facades as a new technological-operational system of transparent exterior walls. Especially of high-rise buildings, which with its operating modes ingeniously uses a renewable source of solar energy to reduce the energy needs of the building. The basic precondition for the correct function of the double skin facade is its functional aerodynamics in any climatic conditions of the outdoor climate. In the critical state of windlessness, the aerodynamic quantification of a double skin facade is the total aerodynamic resistance of the cavity, which consists of the aerodynamic frictional resistances along the length of the air flow line and local aerodynamic resistances of the cavity. The article analyses the functional aerodynamics on two frequented types of double skin facades with a narrow type and corridor type cavity. At the end it confronts functional aerodynamics with the results of their temperature, aerodynamic and energy regime obtained from in-situ experiments.

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Wang, Junzhe. "Analysis of the Principle and Applications of Aerodynamics of High-speed Railway". Highlights in Science, Engineering and Technology 72 (15.12.2023): 530–35. http://dx.doi.org/10.54097/ymwbxx75.

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With the advancement of science and technology, the railway has become an important breakthrough. Railroads can transport goods and carry people. Aerodynamics has a huge connection to the study of the high-speed railways. On this basis, the subject of this paper is the principle and application analysis of high-speed railway aerodynamics. To be specific, this study introduces the formulas and principles related to aerodynamics, and how some formulae are used in high-speed railways. The research searches for literature related to railway and aerodynamics and finds the current development status of high-speed railway. The paper explains how aerodynamics affect high-speed rail, the way to transform high-speed railways with aerodynamic knowledge. Contemporarily, there are many methods to carry out the simulation and tunnel experiments. This study also introduces some special experiments to solve special problems about high-speed railway. According to the analysis, there are still many aerodynamic problems that people need to solve, and there is room for improvement in high-speed railways.

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Ni, Runzhou. "Research on the application of aerodynamic in cycling". Theoretical and Natural Science 12, nr 1 (17.11.2023): 227–32. http://dx.doi.org/10.54254/2753-8818/12/20230478.

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As a bicycle moves, the rider feels air resistance, which affects speed and the rider's energy expenditure. In cycling races, where the main focus is on increasing speed, modifications to the design of the bike, optimization of the bike's materials, and adjustments to the riding position are often utilized to increase speed and reduce energy expenditure. These optimizations are based on aerodynamic principles, which is one of the practical applications of aerodynamic developments. Therefore, the influence of aerodynamics is becoming more and more important in today's bicycle racing. In this paper, the application of aerodynamics in cycling is studied and analyzed through theoretical analysis and literature review. Based on the experimental study of aerodynamics, the optimization of various parts of the bicycle is analyzed to give riders the advantage and help them to increase their speed. Provides the reader with an initial understanding of the application of aerodynamics in cycling.

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Žilinský, Juraj, i Milan Vanc. "Applied Aerodynamics in Building". Advanced Materials Research 855 (grudzień 2013): 164–67. http://dx.doi.org/10.4028/www.scientific.net/amr.855.164.

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Development of new materials, high strength concrete, steels, composites, new construction techniques and procedures put the Development of new materials, high strength concrete, steels, composites, new construction techniques and procedures put the foundations of a new generation of buildings. With the advent of advanced computer technology, using the finite element method engineers and architects plan and construct buildings that are, high, flexible, thin and lightweight. These buildings, however, are burdened by aerodynamic forces, whose source is wind. Just the action of aerodynamic forces adversely affects their ability to traffic, reducing safety and durability. It is therefore necessary to provide high flexibility structures and maintain their safety. This can only be achieved by means of applied aerodynamics using various types of passive and active components to optimize aerodynamics of buildings.

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Toet, W. "Aerodynamics and aerodynamic research in Formula 1". Aeronautical Journal 117, nr 1187 (styczeń 2013): 1–26. http://dx.doi.org/10.1017/s0001924000007739.

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AbstractThis paper will address the engineering performance differentiators for an F1 car and highlight the difference aerodynamics can make to that performance. It will also consider some basic aerodynamic challenges and the main tools used for aerodynamic exploration by teams.

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Rozprawy doktorskie na temat "Aerodynamics"

Vančura, Jan. "Výpočet aerodynamiky závodního automobilu". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2008. http://www.nusl.cz/ntk/nusl-228231.

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The main subject of this diploma thesis is computation of race car aerodynamics. It describes composition method of CFD model with utilization of 3D scanner ATOS and CAD software Pro Engineer. During creating this diploma thesis were found influences of additional aerodynamics components of racing car on globally axle loads.

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Lång, Marcus. "CFD-Method for 3D Aerodynamic Adjoint Simulations : For External Automotive Aerodynamics". Thesis, Linköpings universitet, Mekanisk värmeteori och strömningslära, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-158624.

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Today’s rules and regulations regarding emissions from combustion vehicles are very strict and the travel range per tank and/or charge, especially for electric vehicles, is a crucial factor which will always be considered by the customers. Hence, automotive manufacturers strive to boost fuel and battery economy. This can, to a great extent, be done by improving the aerodynamics of the vehicle for lower drag. The conventional CFD process for aerodynamic development is relatively time consuming and there is rarely enough timeor resources to find the optimal design in all regions of the vehicle. Hence, the adjoint solver was investigated to make the aerodynamic development process more efficient by providing sensitivities of the geometry with respect to drag force. The adjoint solver was investigated both through a literature review as well as by performing CFD and adjoint simulations. The CFD and adjoint simulations were performed using Fluent 2019 R1 and the realizable k-ε turbulence model. It was found that it is important to monitor surface sensitivities during the solution in addition to the adjoint residuals to assess convergence of the adjoint simulation. It is also recommended to analyse regions of high residuals in the domain to ensure that they are far away from the surface(s) of interest. Investigations regarding different stabilization schemes as well different meshes for the adjoint solver were performed. It was concluded that the residual minimization scheme (RMS) is the preferred stabilization scheme. It was found that a coarser mesh can be used to reduce localized transient behaviour if the adjoint solver has trouble converging. It was found that a simplified model of a fully detailed car geometry is necessary to reduce the complexity and the resolution of the mesh to be able to use the RMS and to avoid local instabilities. A proposed CFD and adjoint procedure with guidelines and recommendation was developed.

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Poláš, Maroš. "Experimentální identifikace aerodynamických vlastností vozidla jízdní zkouškou". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2017. http://www.nusl.cz/ntk/nusl-319863.

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This thesis deals with road loads, coastdown tests and evaluation of measured data. Thesis consists of two main parts: theoretical and computational. The first part describes road loads with focus on aerodynamic drag and lift force. In the second part, a software tool for processing the measurement per ISO 10521-1 is designed and lift force measured with running resistance method is calculated.

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McNabb, Michael Lynn. "Development of a cycloidal propulsion computer model and comparison with experiment". Master's thesis, Mississippi State : Mississippi State University, 2001. http://library.msstate.edu/etd/show.asp?etd=etd-08032001-111940.

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Wakeling, James Michael. "Dragonfly aerodynamics". Thesis, University of Cambridge, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.243066.

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Barman, Emelie. "Aerodynamics of Flutter". Thesis, KTH, Mekanik, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-34152.

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The unsteady ow around an aerofoil placed in a uniform ow stream with an angle of attack is investigated, under the assumption of inviscid, incompressible, two-dimensional flow. In particular, a function of the velocity jump over the wake is achieved, where this function depends on the horizontal displacement and time. The aerofoil geometry is represented by two arbitrary functions, one for the upper and one for the lower side of the aerofoil. These functions are dependent on time, hence the aerofoil can perform oscillating movement, which is the case when subjected to utter. The governing equations for the ow are the Euler equations. By assuming thin aerofoil, small angle of attack and that the perturbation of the wake is small, the problem is linearised. It is shown that the linearised Euler equations can be rewritten as the Cauchy-Riemann equations, and an analytic function exists where its real part is the horizontal velocity component and its imaginary part is the vertical velocity component with opposite sign. The ow eld is then investigated in the complex plane by making an appropriate branch cut removing all discontinuities, and with restrictions on the analytic function such that the kinematic and boundary conditions are satis ed. By using Cauchy's integral formula an expression for the anti-symmetric part of the analytic function is achieved. A general expression for the velocity jump over the wake is obtained, which is applied to the speci c case of harmonic oscillations for a symmetric aerofoil. In the end three types of utter is investigated; twisting oscillations around the centre of stiness, vertical oscillation, and aileron flutter.

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Hazby, Hamid Richard. "Centrifugal compressor aerodynamics". Thesis, University of Cambridge, 2011. https://www.repository.cam.ac.uk/handle/1810/252228.

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Potts, Jonathan Roger. "Disc-wing aerodynamics". Thesis, University of Manchester, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.569224.

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Disc-wings are a class of un-powered, axi-symmetric flight vehicles that use spin to achieve acceptably stable flight characteristics. Examples of commonly encountered disc-wings include the Frisbee sports disc, the athletics discus and the clay pigeon. Historically, it appears that most disc-wing designs have been based on trial and error approaches. The main aim of the present work is to develop a theory of flight for spinstabilised disc-wings that can be used to inform the process of their design. This theory of flight is based both on theoretical analysis and experimental data. It is shown from a simple trim and stability analysis that a disc-wing with positive camber will trim at a positive angle of attack. However, for most axi-symmetric crosssectional shapes, the aerodynamic centre is ahead of the centre of the disc (which by definition is the disc centre of gravity). Hence, the static margin is negative and the disc is unstable in pitch. In practice, a disc-wing must be spun in order to fly successfully. The imparted angular momentum due to the spin means that, through precessional effects, the destabilising pitching moments tend to result in a rolling motion rather than a pitching motion. Thus, without spin, a disc-wing would tumble soon after release. With spin however, the discwing will not tumble, instead it tends to exhibit a relatively benign roll to the left or right, depending on the spin direction. The aerodynamic characteristics of various disc-wing geometries based around a Frisbee sports disc are investigated through a series of wind tunnel experiments on a spinning and non-spinning disc. It is shown that the basic lift and drag characteristics are consistent with those expected for a finite wing of the same aspect ratio. The pitching moment characteristic is key to understanding the resulting disc dynamics. A comparison of pitching moment curves is given, for a number of different cross-sectional profiles, some tested as part of the present work and some taken from data found in the literature. It is shown that the Frisbee cross-section is unique in that the pitching moment is zero at around 9° angle of attack, approximately coincident with the angle attack for best lift to drag ratio, and that the disc is approximately neutrally stable in this region. It is these characteristics that enable a typical Frisbee to fly successfully. Spin has almost negligible effect on aerodynamic forces and moments. Force and moment data is supported by surface pressure data, and by on and off surface flow visualisation. Surface pressure data shows that the aerodynamic centre of the Frisbee cross-section is shifted aft by the presence of an aft pressure peak that is not present on other cross-section shapes. The aft pressure peak is a function of both the upper surface geometry and the presence of the cavity on the under surface of the disc. Flow visualisation and pressure data are used to propose a model of disc-wing flow topology that is dependant on the angle of attack and includes leading edge separation and reattachment, recirculating cavity flow and a pair of trailing vortices. To understand further disc-wing flight dynamics and the effect of aerodynamic characteristics, a six-degree of freedom disc-wing simulation model was developed using Matlab. The simulation is validated against published Frisbee trajectory data obtained from free-flight experiments. Flight profiles are also discussed for a number of different launch conditions consistent with a range of typical Frisbee throws. The simulation is also used to demonstrate that with control moments from suitable control effectors, it is possible to generate a number of proscribed manoeuvres, including a spiral turn and a spiral roll.

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Standen, Paul. "Towed vehicle aerodynamics". Thesis, University of Bath, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.311175.

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Zamboni, Giulio. "Fan root aerodynamics". Thesis, University of Cambridge, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.611841.

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Książki na temat "Aerodynamics"

Kuethe, Arnold M. Foundations of aerodynamics: Bases of aerodynamic design. Wyd. 5. New York: J. Wiley, 1998.

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1932-, Chow Chuen-Yen, red. Foundations of aerodynamics: Bases of aerodynamic design. Wyd. 4. New York: Wiley, 1986.

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1932-, Chow Chuen-yen, red. Foundations of aerodynamics: Bases of aerodynamic design. Wyd. 5. New York: Wiley, 1998.

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1932-, Chow Chuen-yen, red. Foundations of aerodynamics: Bases of aerodynamic design. Wyd. 4. New York: Wiley, 1986.

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Liu, Peiqing. Aerodynamics. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-4586-1.

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Discetti, Stefano, i Andrea Ianiro, red. Experimental Aerodynamics. Boca Raton : CRC Press, 2017.: CRC Press, 2017. http://dx.doi.org/10.1201/9781315371733.

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Chanetz, Bruno, Jean Délery, Patrick Gilliéron, Patrick Gnemmi, Erwin R. Gowree i Philippe Perrier. Experimental Aerodynamics. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-35562-3.

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Nørstrud, Helge, red. Sport Aerodynamics. Vienna: Springer Vienna, 2008. http://dx.doi.org/10.1007/978-3-211-89297-8.

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McLean, Doug. Understanding Aerodynamics. Chichester, UK: John Wiley & Sons, Ltd, 2012. http://dx.doi.org/10.1002/9781118454190.

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Gupta, S. C. Aerodynamics airworthiness. Bangalore, India: Interline, 2005.

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Części książek na temat "Aerodynamics"

Pütz, Ralph, i Ton Serné. "Aerodynamik Aerodynamics". W Rennwagentechnik - Praxislehrgang Fahrdynamik, 197–245. Wiesbaden: Springer Fachmedien Wiesbaden, 2017. http://dx.doi.org/10.1007/978-3-658-16102-6_8.

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Trzesniowski, Michael. "Aerodynamik Aerodynamics". W Gesamtfahrzeug, 159–230. Wiesbaden: Springer Fachmedien Wiesbaden, 2017. http://dx.doi.org/10.1007/978-3-658-15537-7_5.

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Trzesniowski, Michael. "Aerodynamik Aerodynamics". W Gesamtfahrzeug, 183–265. Wiesbaden: Springer Fachmedien Wiesbaden, 2019. http://dx.doi.org/10.1007/978-3-658-26696-7_5.

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Pütz, Ralph, i Ton Serné. "Aerodynamik Aerodynamics". W Rennwagentechnik - Praxislehrgang Fahrdynamik, 233–93. Wiesbaden: Springer Fachmedien Wiesbaden, 2019. http://dx.doi.org/10.1007/978-3-658-26704-9_8.

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Trzesniowski, Michael. "Aerodynamik Aerodynamics". W Rennwagentechnik, 125–84. Wiesbaden: Springer Fachmedien Wiesbaden, 2014. http://dx.doi.org/10.1007/978-3-658-04919-5_5.

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Trzesniowski, Michael. "E Aerodynamik Aerodynamics". W Rennwagentechnik, 127–83. Wiesbaden: Vieweg+Teubner Verlag, 2012. http://dx.doi.org/10.1007/978-3-8348-2209-3_5.

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Tewari, Ashish. "Aerodynamics". W Basic Flight Mechanics, 23–41. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-30022-1_2.

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Pozrikidis, C. "Aerodynamics". W Fluid Dynamics, 606–50. Boston, MA: Springer US, 2001. http://dx.doi.org/10.1007/978-1-4757-3323-5_12.

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Seward, Derek. "Aerodynamics". W Race Car Design, 201–26. London: Macmillan Education UK, 2014. http://dx.doi.org/10.1007/978-1-137-03015-3_9.

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Hucho, Wolf-Heinrich, Klaus Hannemann, Jan Martinez Schramm i Charles Williamson. "Aerodynamics". W Springer Handbook of Experimental Fluid Mechanics, 1043–155. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-30299-5_16.

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Streszczenia konferencji na temat "Aerodynamics"

Ghoreyshi, Mehdi, Martiqua Post, Adam Jirasek, Russell Cummings i Keith Bergeron. "Computational Approximation of Nonlinear Unsteady Aerodynamics Using an Aerodynamic Model Hierarchy". W 29th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-3667.

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Novák, Miroslav, i Martin Bugaj. "Simulations of aerodynamics". W Práce a štúdie. University of Žilina, 2021. http://dx.doi.org/10.26552/pas.z.2021.1.18.

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The aim of the paper is to approach the issue of simulations in aerodynamics. To describe the physical rules and basic mathematical equations, which are essential in the use of computing techniques. The paper deals with CFD (Computational Fluid Dynamics) and informations which are necessary for its understanding, the author further describes different software programs used for simulation purposes. By means of analyzing technical papers, the author compares and describes software considering to their practical use. The author also describes the aerodynamic tunnels and clarifies the basic issues related to aerodynamic tunnels and discuss factors that affect the resulting measurement quality. The author deals with methods of measuring individual physical quantities that are the interest of simulation or measurement. At the end of the paper, the author compares the specific aerodynamic tunnels and the possibilities of measurements that aerodynamics tunnels provide.

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Chan, David, Eric Walker, Philip Robinson i Thomas Wilson. "Modeling Powered Aerodynamics for the Orion Launch Abort Vehicle Aerodynamic Database (Invited)". W 29th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-3344.

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WHITEHEAD, JR., ALLEN. "NASP aerodynamics". W National Aerospace Plane Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-5013.

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Wejchert, Jakub, i David Haumann. "Animation aerodynamics". W the 18th annual conference. New York, New York, USA: ACM Press, 1991. http://dx.doi.org/10.1145/122718.122719.

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Birkenstock, David. "Increased Fuel Economy From Powered Aerodynamics and Aerodynamic Pressure Thrust". W 18th AIAA Lighter-Than-Air Systems Technology Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-2864.

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Fulton, Alexander B., Genevieve M. Lipp, Jeffrey D. Reid i Brian P. Mann. "Cycling Aerodynamics: The Effect of Rider Position on Aerodynamic Drag". W ASME 2013 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/imece2013-63488.

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Streszczenie:

Competitive cyclists seek to maximize their efficiency by minimizing the influence of resistive forces. At the high speeds maintained during competition, aerodynamic drag is the primary resistive force. This paper investigates the influence of a cyclist’s body position using models of aerodynamic drag and elucidates the time benefit of various body positions. Mathematical models from prior work, which use cyclist mass and body position angles, have been used to determine the projected frontal area of a cyclist and the aerodynamic drag. Graphical representation of the non-linear relationship between aerodynamic drag and an increasing velocity are also provided. Finally, simulations are produced for a 40 km time trial course, and the results indicate a maximum performance increase of 20.71% due entirely to rider body position when exerting 400 W. We conclude aerodynamic efficiency is crucial in competitive cycling, and its significant correlation with rider body position should not be ignored.

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Askins, Paul, Peter Zell, James Ross, Paul Askins, Peter Zell i James Ross. "Aerodynamic decelerator testing in the National Full-Scale Aerodynamics Complex". W 14th Aerodynamic Decelerator Systems Technology Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1528.

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FARASSAT, F., i M. MYERS. "Aerodynamics via acoustics - Application of acoustic formulas for aerodynamic calculations". W 10th Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1877.

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Huang, Yanxin, i Weihua Su. "Linearization and Analytical Aerodynamic Sensitivity of Unsteady Vortex-Lattice Aerodynamics". W AIAA Scitech 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-1215.

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Raporty organizacyjne na temat "Aerodynamics"

Cole, Julian D. Theoretical Aerodynamics. Fort Belvoir, VA: Defense Technical Information Center, styczeń 1996. http://dx.doi.org/10.21236/ada304107.

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Miller, Miles C. Experimental Aerodynamic Facilities of the Aerodynamics Research and Concepts Assistance Branch. Fort Belvoir, VA: Defense Technical Information Center, luty 1992. http://dx.doi.org/10.21236/ada247489.

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Griffin, D. A., i T. J. McCoy. COE Reductions through Active Aerodynamic Control of Rotor Aerodynamics and Geometry. Office of Scientific and Technical Information (OSTI), grudzień 2008. http://dx.doi.org/10.2172/945953.

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Anderson, Jr, i John D. Hypersonic Aerodynamics Fellowships. Fort Belvoir, VA: Defense Technical Information Center, luty 1991. http://dx.doi.org/10.21236/ada233584.

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Anderson, John D., i Jr. Fellowships in Hypersonic Aerodynamics. Fort Belvoir, VA: Defense Technical Information Center, luty 1988. http://dx.doi.org/10.21236/ada194265.

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Cole, Julian D. Theoretical Aerodynamics, Transonic Flow. Fort Belvoir, VA: Defense Technical Information Center, luty 1988. http://dx.doi.org/10.21236/ada196247.

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Johari, Hamid, i K. J. Desabrais. Aerodynamics of Parachute Opening. Fort Belvoir, VA: Defense Technical Information Center, lipiec 2002. http://dx.doi.org/10.21236/ada411095.

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Graham, Sean, i Patrick Bigatel. Freight Wing Trailer Aerodynamics. Office of Scientific and Technical Information (OSTI), październik 2004. http://dx.doi.org/10.2172/850252.

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Shirahase, Toru, i Akiyoshi Oku. Racing Car Aerodynamics Development. Warrendale, PA: SAE International, maj 2005. http://dx.doi.org/10.4271/2005-08-0387.

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Smith, Justin. Sandia Parallel Aerodynamics Reentry Code (SPARC) ? the Future of Production and Research Aerodynamics. Office of Scientific and Technical Information (OSTI), sierpień 2020. http://dx.doi.org/10.2172/1648402.

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