Academic literature on the topic 'Airplanes Aerodynamics'

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Journal articles on the topic "Airplanes Aerodynamics"

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bin Abu Bakar, Mohd Ridh, Bambang Basuno, and Sulaiman Hasan. "Aerodynamics Analysis on Unsymmetrical Fuselage Models." Applied Mechanics and Materials 315 (April 2013): 273–77. http://dx.doi.org/10.4028/www.scientific.net/amm.315.273.

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The large commercial passengers airplanes are mostly designed to have symmetrical body with respect to the longitudinal axis. However for small passengers airplanes or for the airplane designed as UAV plat form is normally having an unsymmetrical fuselage. The aerodynamics characteristics fuselage may give a strong influence to the overall aerodynamics characteristics of the airplane. The present work investigates the aerodynamics characteristics of the unsymmetrical fuselage with respect to the longitudinal axis. The fuselage assumed to have circular cross section and the coordinate of the fu
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Secco, Ney Rafael, and Bento Silva de Mattos. "Artificial neural networks to predict aerodynamic coefficients of transport airplanes." Aircraft Engineering and Aerospace Technology 89, no. 2 (2017): 211–30. http://dx.doi.org/10.1108/aeat-05-2014-0069.

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Purpose Multidisciplinary design frameworks elaborated for aeronautical applications require considerable computational power that grows enormously with the utilization of higher fidelity tools to model aeronautical disciplines like aerodynamics, loads, flight dynamics, performance, structural analysis and others. Surrogate models are a good alternative to address properly and elegantly this issue. With regard to this issue, the purpose of this paper is the design and application of an artificial neural network to predict aerodynamic coefficients of transport airplanes. The neural network must
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Wegener, Peter P., and Tom D. Crouch. "What Makes Airplanes Fly? History, Science and Applications of Aerodynamics." American Journal of Physics 61, no. 3 (1993): 285. http://dx.doi.org/10.1119/1.17255.

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Karpuk, Stanislav, Snorri Gudmundsson, and Vladimir Golubev. "Feasibility Study of a Multi-Purpose Aircraft Concept with a Leading-Edge Embedded Cross-Flow Fan." Unmanned Systems 08, no. 01 (2020): 21–32. http://dx.doi.org/10.1142/s2301385020500028.

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The research presented focuses on investigating the use of Cross-Flow Fan (CFF) as a high-lift device for a Short Take-off and Landing (STOL) aircraft. The wing-embedded fan performance analysis is mostly addressed from an aerodynamic perspective and focuses on using such Active Flow Control (AFC) technology in the conceptual aircraft design process. In particular, the design trade study of an aircraft featuring the fan as a high-lift device applied to a conceptual design of a medium-range multi-purpose aircraft is performed. A sensitivity analysis is employed to investigate the impact of the
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Mahdal, Miroslav, Josef Dobeš, and Milada Kozubková. "Measurement of Aerodynamic and Acoustic Quantities Describing Flow around a Body Placed in a Wind Tunnel." Measurement Science Review 19, no. 1 (2019): 20–28. http://dx.doi.org/10.2478/msr-2019-0004.

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Abstract Aerodynamically generated noise affects passenger comfort in cars, high-speed trains, and airplanes, and thus, automobile manufacturers aim for its reduction. Investigation methods of noise and vibration sources can be divided into two groups, i.e. experimental research and mathematical research. Recently, owing to the increase in computing power, research in aerodynamically generated noise (aero-acoustics) is beginning to use modern methods such as computational fluid dynamics or fluid-structure interaction. The mathematical model of turbulent flow is given by the system of partial d
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Wiriadidjaja, Surjatin, Amzari Zhahir, Zahratu Hilall Mohamad, Shikin Razali, Ahmad Afifi Puaat, and Mohamed Tarmizi Ahmad. "Wing-in-ground-effect craft: A case study in aerodynamics." International Journal of Engineering & Technology 7, no. 4.13 (2018): 5. http://dx.doi.org/10.14419/ijet.v7i4.13.21319.

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A wing-in-ground-effect (WIGE) crafts can be deployed to fly by utilizing the ground effect, which is a natural phenomenon known to improve the efficiency of airplanes during take-off and landing approaches. In contrast, WIGE craft is not commercially viable for public transport mainly due to the difficulties in controlling its longitudinal stability. As an attempt to support the development of WIGE crafts, this paper presents a case study in aerodynamics based on certain published reports, specifically to reveal the available research data that are considered of interest and can be used as a
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Balasubramaniam, Ramesh, and Anatol G. Feldman. "Some robotic imitations of biological movements can be counterproductive." Behavioral and Brain Sciences 24, no. 6 (2001): 1050–51. http://dx.doi.org/10.1017/s0140525x01220123.

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It is proposed here that Webb's ideas about robots as possible models of animals need some rethinking. In our view, even though widely used biorobotics strategies are fairly successful at reproducing the macroscopic behavior of biological systems, there are still several problems unresolved on the side of robotics as well as biology. Both mathematical and hardware-like robotics models should be feasible physiologically. Control principles elaborated in robotics are not necessarily applied to biological control systems. Although observations of flying birds inspired aerodynamics and thus modern
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Rahmati, Seyed Mohammadali, and Alireza Karimi. "A Nonlinear CFD/Multibody Incremental-Dynamic Model for A Constrained Mechanism." Applied Sciences 11, no. 3 (2021): 1136. http://dx.doi.org/10.3390/app11031136.

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Numerical analysis of a multibody mechanism moving in the air is a complicated problem in computational fluid dynamics (CFD). Analyzing the motion of a multibody mechanism in a commercial CFD software, i.e., ANSYS Fluent®, is a challenging issue. This is because the components of a mechanism have to be constrained next to each other during the movement in the air to have a reliable numerical aerodynamics simulation. However, such constraints cannot be numerically modeled in a commercial CFD software, and needs to be separately incorporated into models through the programming environment, such
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Morino, L., B. K. Bharadvaj, M. I. Freedman, and K. Tseng. "Boundary integral equation for wave equation with moving boundary and applications to compressible potential aerodynamics of airplanes and helicopters." Computational Mechanics 4, no. 4 (1989): 231–43. http://dx.doi.org/10.1007/bf00301382.

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Olejnik, Aleksander, Łukasz Kiszkowiak, and Adam Dziubiński. "Aerodynamic analysis of General Aviation airplanes using computational fluid dynamics methods." Mechanik 90, no. 8-9 (2017): 802–4. http://dx.doi.org/10.17814/mechanik.2017.8-9.118.

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The problems of an aircraft aerodynamic analysis based on the example of Very Light Aeroplanes and Very Light Jet category airplanes have been presented. A numerical calculations using finite volume method implemented in specialized software were performed. A method of preparing a numerical model of an airplane and the aerodynamic analysis methodology have been presented. An influence of an airplane propulsion on aerodynamic characteristics have been analyzed. A results have been shown in the graphs form of aerodynamic force and moment components as function of angle of attack.
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Dissertations / Theses on the topic "Airplanes Aerodynamics"

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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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Detwiler, Kevin P. "Reduced fan noise radiation from a supersonic inlet." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-09192009-040457/.

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Fleming, Jonathan Lee. "An experimental study of a turbulent wing-body junction and wake flow." Thesis, This resource online, 1991. http://scholar.lib.vt.edu/theses/available/etd-08222009-040300/.

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Wolfe, Douglas E. "Airplane dynamic modeling and automatic flight control design." Master's thesis, This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-01202010-020132/.

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Mazza, Joseph R. "An experimental and computational aerodynamic investigation of a low-canard high-wing aircraft design." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-03172010-020720/.

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Peterson, Kevin G. "Rolling moments and aerodynamic time scales for a model with a moving nose stagnation point." Thesis, Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/12048.

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Chiu, Yih-wan Danny. "Convergence of discrete-vortex induced-flow calculations by optimum choice of mesh." Diss., Georgia Institute of Technology, 1988. http://hdl.handle.net/1853/12390.

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Hazarika, Neep. "An inverse method for blended wing-body configurations." Diss., Georgia Institute of Technology, 1988. http://hdl.handle.net/1853/12498.

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Worley, John C. Ahmed Anwar. "Yaw-roll coupled oscillations of a slender delta wing." Auburn, Ala, 2008. http://repo.lib.auburn.edu/EtdRoot/2008/SUMMER/Aerospace_Engineering/Thesis/Worley_John_37.pdf.

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Yu, Chao. "An acoustic intensity-based method and its aeroacoustic applications." Diss., Connect to online resource - MSU authorized users, 2008.

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Books on the topic "Airplanes Aerodynamics"

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Alban, C. M. Homebuilder's aerodynamics. C.M. Alban, 1985.

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Aerodynamics for engineering students. 6th ed. Butterworth-Heinemann, 2012.

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Aerodynamics, aeronautics, and flight mechanics. 2nd ed. Wiley, 1995.

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Aerodynamics, aeronautics and flight mechanics. 2nd ed. Wiley, 1995.

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McCormick, B. W. Aerodynamics, aeronautics and flight mechanics. 2nd ed. Wiley, 1995.

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Gupta, S. C. Aerodynamics airworthiness. Interline, 2005.

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Why do airplanes fly? PowerKids Press, 2010.

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Craig, Gale M. Stop abusing Bernoulli!: How airplanes really fly. Regenerative Press, 1997.

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Aerodynamics for naval aviators. Aviation Supplies & Academics, 1992.

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Hurt, Hugh H. Aerodynamics for naval aviators. Skyhorse Pub., 2012.

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Book chapters on the topic "Airplanes Aerodynamics"

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Wegener, Peter P. "Turning to Aerodynamics." In What Makes Airplanes Fly? Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_6.

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Wegener, Peter P. "Turning to Aerodynamics." In What Makes Airplanes Fly? Springer New York, 1997. http://dx.doi.org/10.1007/978-1-4612-2254-5_6.

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Palocz-Andresen, Michael. "Aerodynamics of Vehicles and Airplanes, and Hydrodynamics of Ships." In Decreasing Fuel Consumption and Exhaust Gas Emissions in Transportation. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-11976-7_7.

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Wegener, Peter P. "Aerodynamic Drag." In What Makes Airplanes Fly? Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_7.

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Wegener, Peter P. "Aerodynamic Lift." In What Makes Airplanes Fly? Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_8.

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Wegener, Peter P. "Aerodynamic Drag." In What Makes Airplanes Fly? Springer New York, 1997. http://dx.doi.org/10.1007/978-1-4612-2254-5_7.

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Wegener, Peter P. "Aerodynamic Lift." In What Makes Airplanes Fly? Springer New York, 1997. http://dx.doi.org/10.1007/978-1-4612-2254-5_8.

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Morino, Luigi, Bala K. Bharadvaj, Marvin I. Freedman, and Kadin Tseng. "BEM for Wave Equation with Boundary in Arbitrary Motion and Applications to Compressible Potential Aerodynamics of Airplanes and Helicopters." In Advanced Boundary Element Methods. Springer Berlin Heidelberg, 1988. http://dx.doi.org/10.1007/978-3-642-83003-7_29.

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Chattot, J. J., and M. M. Hafez. "Glider and Airplane Design." In Theoretical and Applied Aerodynamics. Springer Netherlands, 2015. http://dx.doi.org/10.1007/978-94-017-9825-9_11.

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Frommann, O., and D. Forbrich. "Aerodynamic Optimization of Airplane Wings using Analogy Methods." In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag, 1999. http://dx.doi.org/10.1007/978-3-663-10901-3_23.

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Conference papers on the topic "Airplanes Aerodynamics"

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Ng, Bing Feng, Qiao Mei Kng, Yin Yin Pey, and Jorg Schluter. "On the Aerodynamics of Paper Airplanes." In 27th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-3958.

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Yadlin, Yoram, and Arvin Shmilovich. "Lift Enhancement for Upper Surface Blowing Airplanes." In 31st AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-2796.

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Moitra, Anutosh. "CFD evaluation of the effects of stall control devices and transition tapes on stall behavior of airplanes." In 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-3245.

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Petrović, Igor, Sean P. Shea, Ian P. Smith, Franc Kosel, and Pier Marzocca. "Numerical and Experimental Investigation of Membrane Wing for Micro Aerial Vehicle Applications." In ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/imece2014-38581.

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Micro-Air-Vehicles (MAV) flight regimes differs significantly from larger scales airplanes. They are operating at low Reynolds numbers of approximate 104, cruising at speed about 12m/s, and are capable of agile maneuvers in limited space environment. They are compact and easily stowable to facilitate transportation. However, due to the small size, they are usually more vulnerable to the wind gusts with significant complexities associated to their flight mechanics, stability and control, which also makes difficult to quantify flight qualities and performances. Furthermore, complex aerodynamics
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Khamedov, Ruslan, Ruslan Baitlessov, and Luis Rojas-Solórzano. "CFD Study of Effects of Boundary Layer Suction on Transonic SC(2)-0714 Airfoil Performance." In ASME 2017 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/imece2017-70848.

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The complete understanding of the aerodynamics of wings and blades under transonic conditions represents a substantial challenge in the design of modern airplanes and turbomachinery. Transonic flow over airfoils may result in appearance of shock waves, which lead to increase in drag if not properly considered during the design stage. Therefore, it is a major challenge to design transonic airfoils such that potential appearance of shock waves is foreseen and negative drag effects are minimized. This paper presents the computational study of the SC(2)-0714 airfoil, focusing on its aerodynamics c
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VASSBERG, JOHN, and KATHLEEN DAILEY. "AIRPLANE - Experiences, benchmarks and improvements." In 8th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2998.

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Dimino, Ignazio, Salvatore Ameduri, and Antonio Concilio. "Preliminary Failure Analysis and Structural Design of a Morphing Winglet for Green Regional Aircraft." In ASME 2018 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/smasis2018-8236.

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Aircraft wing design optimization typically requires the consideration of many competing factors accounting for both aerodynamics and structures. To address this, research on morphing aircraft has shown its potential by providing large benefits on aircraft performance. In particular, by adapting wing lift distribution, morphing winglets are capable to improve aircraft aerodynamic efficiency in off-design conditions and reduce wing loads at critical flight points. For those reasons, it is expected that these devices will be applied to the aircraft of the very next generation. In the study herei
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Durán Ferreras, Alfonso. "Aerodynamic Modeling of Variable Sweep Airplanes." In AIAA Modeling and Simulation Technologies Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-5687.

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SADREHAGHIGHI, IDEEN, ROBERTE SMITH, and SURENDRA TIWARI. "Grid and aerodynamic sensitivity analyses of airplane components." In 11th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3475.

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KUBRYNSKI, K. "Two-point optimization of complete three-dimensional airplane configuration." In 10th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2618.

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