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Relevant bibliographies by topics / Aircraft wake

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Academic literature on the topic 'Aircraft wake'

Author: Grafiati

Published: 7 July 2024

Last updated: 31 July 2025

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Journal articles on the topic "Aircraft wake"

1

Pan, Weijun, Zhengyuan Wu, and Xiaolei Zhang. "Identification of Aircraft Wake Vortex Based on SVM." Mathematical Problems in Engineering 2020 (May 12, 2020): 1–8. http://dx.doi.org/10.1155/2020/9314164.

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The aircraft wake vortex has important influence on the operation of the airspace utilization ratio. Particularly, the identification of aircraft wake vortex using the pulsed Doppler lidar characteristics provides a new knowledge of wake turbulence separation standards. This paper develops an efficient pattern recognition-based method for identifying the aircraft wake vortex measured with the pulsed Doppler lidar. The proposed method is outlined in two stages. (i) First, a classification model based on support vector machine (SVM) is introduced to extract the radial velocity features in the wi

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2

Pan, Weijun, Yuanfei Leng, Haoran Yin, and Xiaolei Zhang. "Identification of Aircraft Wake Vortex Based on VGGNet." Wireless Communications and Mobile Computing 2022 (June 18, 2022): 1–10. http://dx.doi.org/10.1155/2022/1487854.

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The exploration of information for aircraft wake vortex enables us to obtain new knowledge of wake turbulence separation standards. Traditional manual methods cannot work satisfactorily for the identification of great number of wake vortex data with high accuracy. Fortunately, the LiDAR intensity data can be explained by integrating LiDAR products with the strategies of computer vision. To overcome the limitation of traditional manual methods, this paper is aimed at developing an automatic method to identify a given set of wake vortices from various aircrafts. The main innovation works are out

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3

Filippov, R. N., and E. A. Titova. "Effect of the Wake Vortex on the Mutual Safety of Winged Aircraft Following the Same Route." Proceedings of Higher Educational Institutions. Маchine Building, no. 10 (739) (October 2021): 65–73. http://dx.doi.org/10.18698/0536-1044-2021-10-65-73.

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The wake vortex consists mainly of two vortices, which are formed when the stream flows around the wings of an aircraft. A semi-empirical model of a stable vortex wake is proposed and analyzed. The model allows describing the velocity field in a vortex, depending on the characteristics of the aircraft generator, as well as assessing the effect of the vortex on the subsequent aircraft. Statistical modeling was carried out to determine the safe interval between the aircrafts for the characteristic sections of the trajectory. When moving over the sea, a straight-line route, a trajectory with turn

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Tomaszewski, Jessica M., Julie K. Lundquist, Matthew J. Churchfield, and Patrick J. Moriarty. "Do wind turbines pose roll hazards to light aircraft?" Wind Energy Science 3, no. 2 (2018): 833–43. http://dx.doi.org/10.5194/wes-3-833-2018.

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Abstract. Wind energy accounted for 5.6 % of all electricity generation in the United States in 2016. Much of this development has occurred in rural locations, where open spaces favorable for harnessing wind also serve general aviation airports. As such, nearly 40 % of all United States wind turbines exist within 10 km of a small airport. Wind turbines generate electricity by extracting momentum from the atmosphere, creating downwind wakes characterized by wind-speed deficits and increased turbulence. Recently, the concern that turbine wakes pose hazards for small aircraft has been used to lim

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Pan, Weijun, Yuming Luo, Shuai Han, and Hao Wang. "Large Eddy Simulation Research on the Evolution Mechanism of Aircraft Wake Influenced by Cubic Obstacle." Geofluids 2022 (June 24, 2022): 1–17. http://dx.doi.org/10.1155/2022/1324531.

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Aircraft wake is a kind of intense air movement, and the study of its generation, development, and dissipation law is of great significance to the flight safety. There are abundant researches on the evolution of aircraft wakes affected by weather and ground effects; however, there are few studies on the influence of a single obstacle on the evolution of aircraft wake. In this article, in order to explore the influence of a single obstacle on the evolution of aircraft wake, firstly, we develop a computational fluid dynamics-based method of simulation of aircraft wake affected by cubic obstacle

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Whitehouse, G. R., and R. E. Brown. "Modelling a helicopter rotor’s response to wake encounters." Aeronautical Journal 108, no. 1079 (2004): 15–26. http://dx.doi.org/10.1017/s0001924000004954.

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In recent years, various strategies for the concurrent operation of fixed-and rotary-wing aircraft have been proposed as a means of increasing airport capacity. Some of these strategies will increase the likelihood of encounters with the wakes of aircraft operating nearby. Several studies now exist where numerical simulations have been used to assess the impact of encounters with the wakes of large transport aircraft on the safety of helicopter operations under such conditions. This paper contrasts the predictions of several commonly-used numerical simulation techniques when each is used to mo

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Pan, Weijun, Zirui Yin, Yuming Luo, Anding Wang, and Yuanjing Huang. "Dynamic Aircraft Wake Separation Based on Velocity Change." Aerospace 9, no. 11 (2022): 633. http://dx.doi.org/10.3390/aerospace9110633.

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Traditional research on static wake-vortex reduction usually considers only the influence of external environmental factors, while ignoring the dynamic change in an aircraft’s flight state. In order to solve this problem, this paper proposes a method to reduce separation using dynamic wake information based on changes in flight velocity. Firstly, relying on the wake-vortex generation and dissipation model, the initial circulations and dissipation parameters of the wake vortex at different aircraft velocities are calculated. Then, the complete evolution process of the wake vortex generated by d

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Ma, Yuzhao, Jiangbei Zhao, Haoran Han, Pak-wai Chan, and Xinglong Xiong. "Aircraft Wake Recognition Based on Improved ParNet Convolutional Neural Network." Applied Sciences 13, no. 6 (2023): 3560. http://dx.doi.org/10.3390/app13063560.

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The occurrence of wake can pose a threat to the flight safety of aircraft and affect the runway capacity and airport operation efficiency. To effectively identify aircraft wake, this paper proposes a novel convolutional neural network (CNN) method of aircraft wake recognition based on the improved parallel network (ParNet). Depthwise separable convolution (DSC) was introduced into the ParNet to make the wake recognition model lightweight. In addition, the convolutional block attention module (CBAM) was introduced into the wake recognition model to improve the capacity of the model to extract t

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LU, Fei, Jian ZHANG, Erli ZHAO, and Jingjie TENG. "Study on Longitudinal Collision Risk of Closely Spaced Parallel Runways Paired Approach." Promet - Traffic&Transportation 37, no. 2 (2025): 404–20. https://doi.org/10.7307/ptt.v37i2.748.

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This study asserts that paired aircraft can withstand specific wake turbulence levels and explores the longitudinal collision risk in closely spaced parallel runway approaches. The goal is to enhance the safety margin of the paired approach and allow for more flexible implementation. Based on QAR data, a theoretical spacing model for paired aircraft and a probability distribution of acceleration error are established to facilitate the analysis of the actual spacing of paired aircraft. Wake turbulence attenuation is modelled using large eddy simulation, creating a vortex attenuation model. Draw

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Pan, Wei-Jun, Yuan-Fei Leng, Tian-Yi Wu, Ya-Xing Xu, and Xiao-Lei Zhang. "Conv-Wake: A Lightweight Framework for Aircraft Wake Recognition." Journal of Sensors 2022 (July 15, 2022): 1–11. http://dx.doi.org/10.1155/2022/3050507.

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The recognition of aircraft wake vortex can provide an indicator of early warning for civil aviation transportation safety. In this paper, several wake vortex recognition models based on deep learning and traditional machine learning were presented. Nonetheless, these models are not completely suitable owing to their dependence on the visualization of LiDAR data that yields the information loss of in reconstructing the behavior patterns of wake vortex. To tackle this problem, we proposed a lightweight deep learning framework to recognize aircraft wake vortex in the wind field of Shenzhen Baoan

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Dissertations / Theses on the topic "Aircraft wake"

1

Stephan, Anton. "Wake vortices of landing aircraft." Diss., Ludwig-Maximilians-Universität München, 2014. http://nbn-resolving.de/urn:nbn:de:bvb:19-167566.

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Bertényi, Tamás. "Merger of aircraft wake vortices." Thesis, University of Cambridge, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.620288.

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Rodenhiser, Rebecca J. "An Ultrasonic Method for Aircraft Wake Vortex Detection." Digital WPI, 2005. https://digitalcommons.wpi.edu/etd-theses/1004.

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"This thesis documents the experimental proof of concept study for an ultrasonic method of wake vortex detection. A new acoustic technique is utilized to measure the circulation produced in the wake of lift-generating aircraft. Ultrasonic signals are transmitted in a path around the wake vortex, and are used to determine the average in-line velocity component along the acoustic path. It is shown herein that this velocity component is directly proportional to the net circulation value within the acoustic path. This is the first study to take this methodology and implement it in a realistic airp

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Rodenhiser, Rebecca J. "An ultrasonic method for aircraft wake vortex detection." Link to electronic thesis, 2004. http://www.wpi.edu/Pubs/ETD/Available/etd-083105-160931/.

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Marles, David. "Effect of an axial jet aircraft wake vortices." Thesis, University of Bath, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.488899.

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An experimental study has been performed to evaluate the effect of a cold axial jet on a variety of typical aircraft wake vortex systems in the near-field. This research attempted to alleviate the vortex hazard imposed on trailing aircraft, which is especially important in the crowded skies around airfields.

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Andronache, Constantin. "A study of aerosol interactions in aircraft wake and background atmosphere." Diss., Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/26008.

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Stephan, Anton [Verfasser], and George C. [Akademischer Betreuer] Craig. "Wake vortices of landing aircraft / Anton Stephan. Betreuer: George C. Craig." München : Universitätsbibliothek der Ludwig-Maximilians-Universität, 2014. http://d-nb.info/1049393155/34.

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Roa, Perez Julio Alberto. "Development of Aircraft Wake Vortex Dynamic Separations Using Computer Simulation and Modeling." Diss., Virginia Tech, 2018. http://hdl.handle.net/10919/96199.

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This dissertation presents a research effort to evaluate wake vortex mitigation procedures and technologies in order to decrease aircraft separations, which could result in a runway capacity increase. Aircraft separation is a major obstacle to increasing the operational efficiency of the final approach segment and the runway. An aircraft in motion creates an invisible movement of air called wake turbulence, which has been shown to be dangerous to aircraft that encounter it. To avoid this danger, aircraft separations were developed in the 1970s, that allows time for wake to be dissipated and

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Craig, Margaret Elizabeth. "Trailing-Edge Blowing of Model Fan Blades for Wake Management." Thesis, Virginia Tech, 2005. http://hdl.handle.net/10919/30886.

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Model fan blades designed to implement the wake management technique of trailing-edge blowing were tested in a linear cascade configuration. Measurements were made on two sets of blowing blades installed in the Virginia Tech low-speed linear cascade wind tunnel. The simple blowing blades were identical to the baseline GE Rotor B blades, aside from a slight difference in trailing-edge thickness, a set of internal flow passages, and a blowing slot just upstream of the trailing-edge on the suction side of the blade. The Kuethe vane blades were also slightly thicker at the trailing-edge, and ha

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Schroeder, Nataliya. "Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations." Thesis, Virginia Tech, 2011. http://hdl.handle.net/10919/40924.

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Wake vortices pose a threat to a following aircraft, because they can induce a roll and compromise the safety of everyone on board. Caused by a difference in pressure between the upper and the lower part of the wings, these invisible flows of air are a major hazard and have to be avoided by separating the aircraft at considerable distances. One of the known constraints in airport capacity for both departure and arrival operations is the large headway resulting from the wake spacing separation criteria. Reducing wake vortex separations to a safe level between successive aircraft can increase ca

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Books on the topic "Aircraft wake"

1

Hallock, J. N. Aircraft wake vortices: An annotated bibliography (1923-1990). Research and Development Service, U.S. Dept. of Transportation, Federal Aviation Administration, 1991.

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2

C, Miake-Lye R., and Langley Research Center, eds. Stratospheric aircraft exhaust plume and wake chemistry studies. National Aeronautics and Space Administration, Langley Research Center, 1992.

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3

E, Marshall Robert. Radar reflectivity in wingtip-generated wake vortices. National Aeronautics and Space Administration, Langley Research Center, 1997.

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4

Blackmore, Paul. Slate and tile roofs: Avoiding damage from aircraft wake vortices. CRC, 2002.

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5

Center, Langley Research, ed. Feasibility of detecting aircraft wake vortices using passive microwave radiometers. National Aeronautics and Space Administration, Langley Research Center, 1993.

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6

Center, Langley Research, ed. Characterizing the wake vortex signature for an active line of sight remote sensor. Radar Systems Laboratory, Electrical and Computer Engineering Dept., Clemson University, 1994.

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7

Severin, Theresa Ann. In the wake of the storm: Living beyond the tragedy of Flight 4184. North Cross Press, 2008.

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8

Clark, Richard A. Back to the Bennington: Tales in the wake. Merriam Press, 2010.

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9

D, Campbell S., and Langley Research Center, eds. Wake vortex field measurement program at Memphis, Tennessee: Data guide. National Aeronautics and Space Administration, Langley Research Center, 1997.

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10

Bilanin, Alan J. Interaction of spray aircraft wake with convective surface winds in hilly terrain. USDA Forest Service, 1996.

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Book chapters on the topic "Aircraft wake"

1

Ginevsky, A. S., and A. I. Zhelannikov. "Far Vortex Wake Behind a Turbojet Aircraft." In Foundations of Engineering Mechanics. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-01760-5_4.

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Ginevsky, A. S., and A. I. Zhelannikov. "The Near Vortex Wake Behind a Single Aircraft." In Foundations of Engineering Mechanics. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-01760-5_3.

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3

Tekitchamroon, Theerawit, Watchapon Rojanaratanangkule, and Vejapong Juttijudata. "Breaking the Aircraft Vortex Wake Near the Ground: Mitigation of Turbulence Wake Hazard." In Research Developments in Sustainable Aviation. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-37943-7_31.

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Bellastrada, C., and C. Breitsamter. "Large Transport Aircraft Wake Vortex Affected by Vortex Devices." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-39604-8_1.

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Campos, L. M. B. C., and J. M. G. Marques. "On Aircraft Response and Control During a Wake Encounter." In Progress in Industrial Mathematics at ECMI 2008. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-12110-4_120.

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6

Holzäpfel, Frank, and Thomas Gerz. "Aircraft Wake Vortices: From Fundamental Research to Operational Application." In Atmospheric Physics. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-30183-4_14.

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Chatelain, Philippe, Mattia Gazzola, Stefan Kern, and Petros Koumoutsakos. "Optimization of Aircraft Wake Alleviation Schemes through an Evolution Strategy." In Lecture Notes in Computer Science. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-19328-6_21.

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Lv, Peijian. "A Theoretical Analysis of Boundary Layer Ingestion and Wake Ingestion." In Power-Based Study of Boundary Layer Ingestion for Aircraft Application. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-5497-9_3.

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Ruhland, Johannes, and Christian Breitsamter. "Wake Vortex Analysis on Transport Aircraft Wing Featuring Dynamic Flap Motion." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-79561-0_70.

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Politz, Christina, Benedikt Over, and Tania Kirmse. "The Application of Background Oriented Schlieren Method to Aircraft Wake Vortex Investigations." In Research Topics in Aerospace. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_19.

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Conference papers on the topic "Aircraft wake"

1

Erhard, Racheal, and Juan Alonso. "A Quasi-Prescribed Vortex Wake Method Capturing Rotor Wake Distortion." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1116.

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Prescribed vortex wake methods have historically provided rapid analysis for modeling rotor performance with reasonable accuracy suitable to conceptual and preliminary design. However, determining an appropriate wake geometry requires accurate prescription functions, often relying on empirical data. For distributed electric propulsion (DEP) and electric vertical takeoff and landing (eVTOL) aircraft, interaction effects of installed multi-rotor and rotor-wing systems can introduce significant wake distortion and deflection, which is not captured by a rigid or prescribed wake model. Force-free w

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2

Wachspress, Daniel, Mark Silva, T. Davis, Donald Gaublomme, Eric Hayden, and Tyler Fean. "The Role of Modeling and Simulation in the Mitigation of V-22 Tiltrotor Formation Flight Wake-Induced Roll-off." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11594.

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A real-time free wake modeling capability developed by Continuum Dynamics, Inc. (CDI) was employed by NAVAIR in the mitigation of the wake-induced roll-off hazard experienced by V-22 tiltrotor aircraft while flying in formation in low-speed conversion mode flight. Sub-scale wind tunnel investigations indicated roll-upsets could exceed the control power of the aircraft. PIV measurements from the wind tunnel tests helped characterize the wake and provided the basis for a limited, steady-heading wake encounter simulation capability; however two roll-off events in 2008 occurring in descending turn

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3

Gaifullin, A. M., and G. G. Soudakov. "Aircraft Vortex Wake Dynamics." In World Aviation Congress & Exposition. SAE International, 1996. http://dx.doi.org/10.4271/965547.

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4

"NASA wake vortex research." In Aircraft Design, Systems, and Operations Meeting. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-4004.

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Nelson, Robert, and Eric Jumper. "Aircraft wake vortices and their effect on following aircraft." In AIAA Atmospheric Flight Mechanics Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-4073.

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Chu, Nana, Kam K. H. Ng, Ye Liu, and Kai Kwong Hon. "Analyzing the Potential of Dynamic Aircraft Wake Separation via Data-Driven Aircraft Wake Region Detection." In AIAA AVIATION FORUM AND ASCEND 2024. American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-4249.

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He, Tianyi, Weihua Su, and Zhongquan Charlie Zheng. "Dynamic Load of Urban Air Mobility Aircraft in Wake Vortex of Large Passenger Aircraft." In ASME 2025 Aerospace Structures, Structural Dynamics, and Materials Conference. American Society of Mechanical Engineers, 2025. https://doi.org/10.1115/ssdm2025-152507.

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Abstract This paper investigates the dynamic loads experienced by a UAM (Urban Air Mobility) aircraft encountering a modeled wake vortex generated by a Boeing 737-800. The modeled wake vortex follows the Barnham-Hallock vortex model, characterized by a circular velocity profile. The UAM aircraft is simulated in longitudinal motion, beginning from a trimmed-level flight condition and penetrating the wake vortex with symmetric wing loading. Two flight scenarios are explored: free flight and closed-loop controlled flight. In the controlled scenario, an LQR controller is designed to mitigate the a

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COUSTOLS, Eric, Eike STUMPF, Laurent JACQUIN, Frederic MOENS, Heinrich VOLLMERS, and Thomas GERZ. ""Minimised Wake": a Collaborative Research Programme on Aircraft Wake Vortices." In 41st Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-938.

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Schauerhamer, Daniel G., and Stephen K. Robinson. "Simulating Aircraft Wake Vortices with OVERFLOW." In 33rd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3301.

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Vyshinsky, V. V. "Aircraft Vortex Wake and Airport Capacity." In World Aviation Congress & Exposition. SAE International, 1997. http://dx.doi.org/10.4271/975519.

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Reports on the topic "Aircraft wake"

1

Strickland, J., E. Tadios, and D. Powers. Wind tunnel study of wake downwash behind A 6% scale model B1-B aircraft. Office of Scientific and Technical Information (OSTI), 1990. http://dx.doi.org/10.2172/6839285.

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Doyle, James D., M. A. Shapiro, Robert Gall, and Diana Bartels. Research Aircraft Observations and the Numerical Simulation of a Breaking Gravity Wave Event over Greenland Observed during FASTEX,. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada330935.

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Brodie, Katherine, Brittany Bruder, Richard Slocum, and Nicholas Spore. Simultaneous mapping of coastal topography and bathymetry from a lightweight multicamera UAS. Engineer Research and Development Center (U.S.), 2021. http://dx.doi.org/10.21079/11681/41440.

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A low-cost multicamera Unmanned Aircraft System (UAS) is used to simultaneously estimate open-coast topography and bathymetry from a single longitudinal coastal flight. The UAS combines nadir and oblique imagery to create a wide field of view (FOV), which enables collection of mobile, long dwell timeseries of the littoral zone suitable for structure-from motion (SfM), and wave speed inversion algorithms. Resultant digital surface models (DSMs) compare well with terrestrial topographic lidar and bathymetric survey data at Duck, NC, USA, with root-mean-square error (RMSE)/bias of 0.26/–0.05 and

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