Gotowe bibliografie tematyczne / Aerodynamic loads

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Gotowa bibliografia na temat „Aerodynamic loads”

Autor: Grafiati

Data publikacji: 4 czerwca 2021

Data aktualizacji: 25 lipca 2025

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Artykuły w czasopismach na temat "Aerodynamic loads"

Tomasz Lusiak, Andrej Novak, Martin Bugaj, and Radovan Madlenak. "Assessment of Impact of Aerodynamic Loads on the Stability and Control of the Gyrocopter Model." Communications - Scientific letters of the University of Zilina 22, no. 4 (2020): 63–69. http://dx.doi.org/10.26552/com.c.2020.4.63-69.

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Aerodynamic modelling currently relates to development of mathematical models to describe the aerodynamic forces and moments acting on the aircraft. It is a challenging part of aerodynamics that defines a comprehensive approach to using traditional methods and modern techniques to obtain relevant data. The most complicated task for the aerodynamics and flight dynamics is definition, computation and quantification of the aerodynamic description of an object. This paper presents how to determine the aerodynamic load on a gyrocopter and defines the effect on its stability and control. The first s

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Enciu, K., and A. Rosen. "Aerodynamic modelling of fin stabilised underslung loads." Aeronautical Journal 119, no. 1219 (2015): 1073–103. http://dx.doi.org/10.1017/s0001924000011143.

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AbstractBox-like slung loads exhibit periodic yaw response instabilities, while carried externally by a helicopter. When coupled with the slung load longitudinal and lateral pendulum motions, these instabilities result in significant pendulum oscillations of the load. High amplitude oscillations lead in many cases to the limiting of a load’s flight envelope. Using wind tunnel and flight tests, rear mounted fins were previously demonstrated as efficient means for stabilisation of a problematic load. However, the lack of a proper analytical model of the stabilised load’s aerodynamic characterist

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Abhilash and Joseph Jikhil. "Building Aerodynamics and Shape Optimisation." Journal of Sustainable Construction Engineering and Project Management 6, no. 2 (2023): 1–16. https://doi.org/10.5281/zenodo.7935492.

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<em>This study   is based on the topic building aerodynamics and shape optimization. Usually, the aerodynamic considerations are not taken into account while designing the external shape and orientation of building. The main considerations are architectural considerations, functional requirements and site limitations. As a result, the structures become bluff bodies with strong wind-structure interaction produced loads. These can be reduced by using aerodynamic mitigation techniques and shape optimization procedure. This report reviews the old/recent work on aerodynamic mitigation tec

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Perez-Becker, Sebastian, Francesco Papi, Joseph Saverin, David Marten, Alessandro Bianchini, and Christian Oliver Paschereit. "Is the Blade Element Momentum theory overestimating wind turbine loads? – An aeroelastic comparison between OpenFAST's AeroDyn and QBlade's Lifting-Line Free Vortex Wake method." Wind Energy Science 5, no. 2 (2020): 721–43. http://dx.doi.org/10.5194/wes-5-721-2020.

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Abstract. Load calculations play a key role in determining the design loads of different wind turbine components. To obtain the aerodynamic loads for these calculations, the industry relies heavily on the Blade Element Momentum (BEM) theory. BEM methods use several engineering correction models to capture the aerodynamic phenomena present in Design Load Cases (DLCs) with turbulent wind. Because of this, BEM methods can overestimate aerodynamic loads under challenging conditions when compared to higher-order aerodynamic methods – such as the Lifting-Line Free Vortex Wake (LLFVW) method – leadin

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Tian, Xiao, Wenhui Yan, and Kun Zhang. "Numerical Calculation of 1P Aerodynamic Loads on Aviation Propellers." Journal of Physics: Conference Series 2747, no. 1 (2024): 012043. http://dx.doi.org/10.1088/1742-6596/2747/1/012043.

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Abstract To accurately predict the 1P aerodynamic loads of aviation propellers, this paper established a mathematical model of aviation propeller 1P aerodynamic loads based on the coupling method of blade element theory and momentum theory. Correction methods such as the Prandtl tip correction method and the propeller root correction method were implemented to further improve calculation accuracy. A 1P aerodynamic load calculation procedure was developed based on the mathematical model by using the Matlab software. 1P aerodynamic loads of a three-blade propeller were predicted for three differ

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Jiao, Shuaike, and Jiahong Zheng. "Aerodynamics Analysis of Helicopter Rotor in Flight Test Using Strain Gauge Sensors." Sensors 25, no. 6 (2025): 1911. https://doi.org/10.3390/s25061911.

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The acquisition of aerodynamic loads on helicopter rotors is fundamental to the study of helicopter performance optimization, structural design, flight control, and other aspects. However, at present, aerodynamic loads on rotors are primarily obtained through theoretical calculations, simulation analysis, and wind tunnel tests, with few reports on flight measurements. This paper proposes a method for obtaining helicopter rotor aerodynamic loads by flapping moment measurements in flight with strain gauge sensors. First, strain gauge sensors are installed at different cross-sectional positions o

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Li, Tian, Yifan Li, Lai Wei, and Jiye Zhang. "Study on Lateral Vibration of Tail Coach for High-Speed Train under Unsteady Aerodynamic Loads." Vibration 6, no. 4 (2023): 1048–59. http://dx.doi.org/10.3390/vibration6040061.

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As the speed of high-speed trains increases, the vehicle’s lateral stability steadily deteriorates. There have been observations of abnormal vibrations in the tail car, particularly on certain sections of the railway line. This study built a high-speed train aerodynamic simulation model for a three-car consist, and a multibody dynamics simulation model for an eight-car consist based on numerical simulations of train aerodynamics and multibody dynamics. It investigated both steady and unsteady aerodynamic loads, flow field characteristics, and the dynamic performance of vehicles under varied ae

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Zhang, Xuyao, Congxin Yang, and Shoutu Li. "Influence of the Heights of Low-Level Jets on Power and Aerodynamic Loads of a Horizontal Axis Wind Turbine Rotor." Atmosphere 10, no. 3 (2019): 132. http://dx.doi.org/10.3390/atmos10030132.

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The influence of the heights of low-level jets (LLJs) on the rotor power and aerodynamic loads of a horizontal axis wind turbine were investigated using the fatigue, aerodynamics, structures, and turbulence code. The LLJ and shear inflow wind fields were generated using an existing wind speed spectral model. We found that the rotor power predicted by the average wind speed of the hub height is higher than the actual power in relatively weak and shallow LLJ inflow conditions, especially when the LLJ height is located inside the rotor-swept area. In terms of aerodynamic loads, when the LLJ heigh

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Xiang, Xiao Jun, and Yu Qian. "Numerical Simulation of Unsteady Aerodynamic Loads over an Aircraft." Advanced Materials Research 908 (March 2014): 264–68. http://dx.doi.org/10.4028/www.scientific.net/amr.908.264.

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The unsteady aerodynamic loads are the basic of the aeroelastic. This paper focuses on the computation of the unsteady aerodynamic loads for forced periodic motions under different Mach numbers. The flow is modeled using the Euler equations and an unsteady time-domain solver is used for the computation of aerodynamic loads for forced periodic motions. The Euler equations are discretized on curvilinear multi-block body conforming girds using a cell-centred finite volume method. The implicit dual-time method proposed by Jameson is used for time-accurate calculations. Rigid body motions were trea

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Anil, Mary, and Deepa Varkey. "Recent Progress in Aerodynamics for Aeroelastic Analysis." International Journal for Research in Applied Science and Engineering Technology 10, no. 6 (2022): 2890–93. http://dx.doi.org/10.22214/ijraset.2022.44475.

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Abstract: Aerodynamics has gained considerable popularity in the aerospace industry. Based on the characteristics of a structure, aerodynamic behavior varies from structure to structure. A reliable aeroelastic analysis requires accurate capture of aerodynamic forces. To produce accurate aerodynamic loads, it is necessary to develop an appropriate aerodynamic model. A review of various approaches to aerodynamic modeling for aeroelastic analysis of diverse wing configurations is presented in this paper. The study covers a wide range of finite element software platforms used in the aeroelastic an

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Rozprawy doktorskie na temat "Aerodynamic loads"

Heathcote, Daniel. "Aerodynamic loads control using mini-tabs." Thesis, University of Bath, 2017. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.760920.

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Aircraft encounter increased aerodynamic loads when exposed to gusts, turbulence andmanoeuvres. Currently, these loads are mitigated through the use of ailerons and spoilers to reduce lift, in turn reducing the loads passed to the aircraft structure. However, these actuators are limited in their frequency response and cannot control loads produced by higher frequency events. Therefore, an actuator which can mitigate high frequency oscillatory loads is required, with a deployment reduced frequency, k of up to 1. One such promising load control actuator is the minitab, consisting of a small span

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Mackman, Thomas James. "Surrogate model construction for steady aerodynamic loads." Thesis, University of Bristol, 2013. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.633231.

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An efficient method for predicting steady aerodynamic loads with respect to varying geometric and flow parameters is to use a surrogate model to interpolate or approximate a finite set of Computational Fluid Dynamics (CFD) simulations. Further improvements to the strategy for constructing the surrogate have the potential to provide more accurate predicted values or to reduce the number of simulations required to achieve a model of sufficient quality. This work was originally motivated by the task of providing data for calculating structural loads for civil passenger aircraft, but is directly r

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Spagnolo, Stefano. "Unsteady aerodynamic loads on aircraft landing gear." Thesis, University of Southampton, 2016. https://eprints.soton.ac.uk/397089/.

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The aim of the current work is to improve the accuracy and efficiency of aerodynamic load predictions on landing gear in flight conditions, as part of the UK TSB ALGAAP (Advanced Landing Gear Aero-loads and Aero-noise Prediction) project. To this purpose, both experiments and simulations are performed on simplified landing-gear components. The new geometry presented in this work is a configuration composed of two simplified wheels in tandem. Experimental and numerical results from a single-wheel geometry are used as a baseline for comparison. The models are tested in the University of Southamp

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Kirchmayr, Sara. "Comparison of Aerodynamic Methods for the Computation of Control Surface Loads." Thesis, KTH, Flygdynamik, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-185022.

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This paper presents loads computations for the generic UCAV configuration F19, originally devised by the German Aerospace Center (DLR). Different aerodynamic methods are investigated and their effect on concentrated structural loads is assessed. Design manoeuvres are defined based on the manoeuvre authority. Inertia loads are considered for a preliminary mass breakdown provided by DLR. The loads analysis process is performed both with the DLR and the Airbus Defence and Space (AD&S) aerodynamic data sets. Finally, total loads are generated and the effect of the different underlying aerodyna

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McColl, Chance C. "A matched-harmonic confluence approach to rotor loads prediction with comprehensive application to flight test." Diss., Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/45837.

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Future management of helicopter fleets will be more heavily based on individual component damage tracking and less on legacy usage monitoring (flight parameter-based) methods. This enhances health assessment capabilities by taking into account the actual loads on a component-by-component basis. However, accurate loads prediction in rotating frame components remains a challenge. Even with advanced computational fluid dynamics (CFD) techniques, prediction of the unsteady aerodynamic loads acting on the rotor blades is computationally intensive and problematic in terms of accurate loads predictio

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Spjutare, Christian. "Aerodynamic Loads on External Stores - Saab 39 Gripen : Evaluation of CFD methods for estimating loads on external stores." Thesis, Linköping University, Applied Thermodynamics and Fluid Mechanics, 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-54127.

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<p>External stores mounted on aircraft generate loads which need to be estimated before first takeoff. These loads can be measured in a wind tunnel but since the possible store configurations are basically endless, testing them all is neither economically feasible nor time efficient. Thus, scaling based on geometrical similarity is used. This can, however, be a crude method. Stores with similar geometrical properties can still behave in different ways due to aerodynamic interference caused by adjacent surfaces.</p><p>To improve the scaling performance, this work focuses on investigating two CF

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Mansor, Shuhaimi. "Estimation of bluff body transient aerodynamic loads using an oscillating model rig." Thesis, Loughborough University, 2006. https://dspace.lboro.ac.uk/2134/13208.

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A method for the estimation of transient aerodynamic data from dynamic wind tunnel tests has been developed and employed in the study of the unsteady response of simple automotive type bodies. The experimental setup consists of the test model mounted to the oscillating model facility such that it is constrained to oscillate with a single degree of freedom of pure yawing motion. The yaw position is recorded from a potentiometer and the time response provides the primary measurement. Analysis of the wind-off and wind-on response allows the transient aerodynamic loads to be estimated. The frequen

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Fischer, Tim [Verfasser]. "Mitigation of Aerodynamic and Hydrodynamic Induced Loads of Offshore Wind Turbines / Tim Fischer." Aachen : Shaker, 2012. http://d-nb.info/1052408753/34.

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Berdon, Randall. "Flow structures and aerodynamic loads of a rolling wing in a free stream." Thesis, University of Iowa, 2019. https://ir.uiowa.edu/etd/6705.

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The leading-edge vortex (LEV) is a structure found in unsteady aerodynamics that can alter the forces induced on wings and other rotating structures. This thesis presents an experimental study on LEV development on low aspect-ratio wing rolling in a uniform flow at high angles of attack. The flow structure dynamics of rotating wings in the presence of a free stream are not well understood due to the limited studies under these conditions. In this study, a broad parameter space with varying advance ratio and wing radius of gyration are analyzed using dye-visualizations. In most cases, either a

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Marpu, Ritu Priyanka. "Physics based prediction of aeromechanical loads for the UH-60A rotor." Diss., Georgia Institute of Technology, 2013. http://hdl.handle.net/1853/47661.

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Helicopters in forward flight experience complex aerodynamic phenomena to various degrees. In low speed level flight, the vortex wake remains close to the rotor disk and interacts with the rotor blades to give rise to blade vortex interaction phenomena. In high speed flight, compressibility effects dominate leading to the formation of shocks. If the required thrust is high, the combination of high collective pitch and cyclic pitch variations give rise to three-dimensional dynamic stall phenomena. Maneuvers further exacerbate the unsteady airloads and affect rotor and hub design. The strength

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Książki na temat "Aerodynamic loads"

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Aircraft dynamic loads due to flow separation. AGARD, 1990.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft dynamic loads due to flow separation. AGARD, 1990.

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Dillenius, Marnix F. E. Improvements to the missile aerodynamic prediction code DEMON3. Langley Research Center, 1992.

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Winebarger, Roger M. Loads and motions of an F-106B flying through thunderstorms. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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L, Peterson Randall, and Ames Research Center, eds. Full-scale hingeless rotor performance and loads. National Aeronautics and Space Administration, Ames Research Center, 1995.

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L, Peterson Randall, and Ames Research Center, eds. Full-scale hingeless rotor performance and loads. National Aeronautics and Space Administration, Ames Research Center, 1995.

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L, Peterson Randall, and Ames Research Center, eds. Full-scale hingeless rotor performance and loads. National Aeronautics and Space Administration, Ames Research Center, 1995.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft loads due to turbulence and their impact on design and certification. AGARD, 1994.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft loads due to turbulence and their impact on design and certification. AGARD, 1994.

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Baumann, Peter Helmut. Messung von aerodynamisch bedingten Modellverformungen im Windkanal mittels Moire-Interferometrie. DLR, 1994.

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Części książek na temat "Aerodynamic loads"

Karimirad, Madjid. "Aerodynamic and Hydrodynamic Loads." In Offshore Energy Structures. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-12175-8_9.

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Rutschmann, Sabrina, Klaus Ehrenfried, and Andreas Dillmann. "Aerodynamic Loads Induced by Passing Trains on Track Side Objects." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-03158-3_35.

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Ginevsky, A. S., and A. I. Zhelannikov. "Aerodynamic Loads on Aircraft Encountering Vortex Wakes of Other Aircraft." In Foundations of Engineering Mechanics. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-01760-5_8.

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Zhang, Hui. "Aerodynamic Loads Analysis for a Maneuvering Aircraft in Transonic Flow." In Lecture Notes in Electrical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_15.

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Gan, Edward Chern Jinn, and Salim Mohamed Salim. "Numerical Simulation of the Aerodynamic Loads on Trees During Storms." In Transactions on Engineering Technologies. Springer Netherlands, 2015. http://dx.doi.org/10.1007/978-94-017-9804-4_13.

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Maceri, Franco, and Giuseppe Vairo. "Modelling and Simulation of Long-Span Bridges under Aerodynamic Loads." In Novel Approaches in Civil Engineering. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-45287-4_32.

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Piana, G., A. Manuello, R. Malvano, and A. Carpinteri. "Natural Frequencies of Long-Span Suspension Bridges Subjected to Aerodynamic Loads." In Dynamics of Civil Structures, Volume 4. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-04546-7_45.

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Maktouf, Rania, Majdi Yangui, Rachid Nasri, and Mohamed Haddar. "Investigation of the Aerodynamic Loads of Horizontal Axis Wind Turbines Blade." In Lecture Notes in Mechanical Engineering. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-57324-8_28.

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Schulz, Volker, Roland Stoffel, and Heinz Zorn. "Structural Optimization of 3D Wings Under Aerodynamic Loads: Topology and Shell." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-72020-3_14.

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Poryvaev, Ilya, Aleksandr Semenov, and Marat Safiullin. "Aerodynamic Research of Wind and Snow Loads on the Cylinder Tank Roofs." In Design, Fabrication and Economy of Metal Structures. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-36691-8_81.

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Streszczenia konferencji na temat "Aerodynamic loads"

Koukpaizan, Nicholson, Jagadeesh Movva, Marin Butori, and Marilyn Smith. "Accurate Real-Time Extensible Simulations of Dynamic Bodies." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12109.

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A model-based simulation technique has recently been developed and is being transitioned for use in two-body aerodynamic-dynamic problems of interest (slung loads, airdrops) to the vertical lift community. This model, the Georgia Tech Aerodynamics for Bluff Bodies (GTABB), has been shown to accurately predict the behavior of rectangular loads, validated with both computational fluid dynamics and flight test. This paper presents additional validation of the GTABB solver and its six degree of freedom dynamic modeling tool (6DOF) with flight test on new slung load configurations that are connecte

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Shukla, Dhwanil, Nandeesh Hiremath, and Narayanan Komerath. "Aerial Commuter Architecture Using Slung Loads." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11361.

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Evading traffic congestion by personal flying vehicle is still a far fetched dream. Recent advancements in predicting divergence speeds of slung loads using the Continuous Rotation Method (CRM) of airloads measurement has made is possible to obtain complete aerodynamic load maps of objects. In turn this enables on-the-fly system identification and dynamics predictions to ensure safety and smooth rides with slung loads. A concept is proposed for an air-lift service which can transport people with their personal road vehicles over congested areas. QFD and OEC analyses are used to compare differe

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Marepally, Koushik, James Baeder, Zoren Habana, Jan Goericke, and Ryan Plumley. "Aerodynamic Analysis of Stopped and Stopping Rotors in Lift+Cruise eVTOL Configurations." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-62.

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This study investigates the aerodynamic behavior of lift rotors in a representative lift+cruise electric vertical takeoff and landing (eVTOL) configuration using high-fidelity Computational Fluid Dynamics (CFD) simulations. As lift+cruise concepts gain prominence for Urban Air Mobility (UAM) applications due to their operational simplicity, flight performance, and reduced cruise noise, a detailed understanding of rotor aerodynamics during transition and cruise is critical. CFD analysis was conducted for both slowed rotors at high advance ratios and fully stopped rotors, where traditional predi

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Da Ronch, Andrea, Kenneth J. Badcock, Alex Khrabrov, M. Ghoreyshi, and R. Cummings. "Modeling of Unsteady Aerodynamic Loads." In AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6524.

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Aly, Aly Mousaad, and Girma Bitsuamlak. "Aerodynamic Loads on Solar Panels." In Structures Congress 2013. American Society of Civil Engineers, 2013. http://dx.doi.org/10.1061/9780784412848.137.

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Duda, Benjamin M., Andreas Deurig, Francisco Flores Alvarenga, and Gregory M. Laskowski. "Landing Gear Retraction Under Aerodynamic Loads." In AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-3527.

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Karkehabadi, Reza, and Ray Rhew. "Investigating and Analyzing Applied Loads Higher than Limit Loads." In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-2197.

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BEHR, VANCE. "Measurements of individual parachute loads in a clustered parachute system." In 10th Aerodynamic Decelerator Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-923.

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LAWRENCE, J., J. OLER, and D. ADAMSON. "An experimental investigation of the aerodynamic loads on cambered plates." In 10th Aerodynamic Decelerator Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-935.

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Ray, Eric. "Reconstruction of Orion EDU Parachute Inflation Loads." In AIAA Aerodynamic Decelerator Systems (ADS) Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-1260.

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Raporty organizacyjne na temat "Aerodynamic loads"

Homicz, G. F. Numerical simulation of VAWT stochastic aerodynamic loads produced by atmospheric turbauence: VAWT-SAL code. Office of Scientific and Technical Information (OSTI), 1991. http://dx.doi.org/10.2172/5177561.

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Luttges, Marvin W., Mark S. Miller, Michael C. Robinson, Derek E. Shipley, and David A. Simms. Evidence That Aerodynamic Effects, Including Dynamic Stall, Dictate HAWT Structure Loads and Power Generation in Highly Transient Time Frames. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10177826.

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Fine, Neal, Todd Griffith, and Mario Rotea. Active Aerodynamic Load Control for Wind Turbines. Office of Scientific and Technical Information (OSTI), 2024. http://dx.doi.org/10.2172/2324926.

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Cicolani, Luigi S., Jeffery Lusardi, Lloyd D. Greaves, Dwight Robinson, Aviv Rosen, and Rueben Raz. Flight Test Results for the Motions and Aerodynamics of a Cargo Container and a Cylindrical Slung Load. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada517702.

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Anderson, Evan, Austin Motes, Evan Sproul, Ben Mertz, and Joshua Paquette. Investigation of an Intermittent Binary Control Strategy for Distributed Aerodynamic Control Devices for Load Alleviation in Wind Turbine Blades. Office of Scientific and Technical Information (OSTI), 2024. http://dx.doi.org/10.2172/2429999.

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