Academic literature on the topic 'Ground effect'

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Journal articles on the topic "Ground effect"

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Tran, Thi Thuy. "Effect of Geometric Parameters On Aerodynamic Parameters Of Wings In Ground Effects." International Journal of Research Publication and Reviews 6, no. 4 (2025): 6179–87. https://doi.org/10.55248/gengpi.6.0425.14136.

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Coulliette, C., and A. Plotkin. "Aerofoil ground effect revisited." Aeronautical Journal 100, no. 992 (1996): 65–74. http://dx.doi.org/10.1017/s0001924000027305.

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AbstractSteady state aerofoil ground effect is studied both numerically and analytically. Discrete vortex and linear vortex panel methods are applied to a parabolic arc and symmetric Joukowski aerofoil, respectively. A single vortex model for the flow over the parabolic arc aerofoil is developed. The single vortex model and other analytical solutions, valid either near or far from the ground, are compared with the numerical results. The numerical results are used to delineate the influences of angle of attack, camber and thickness. For small values of camber and angle of attack, normalised lif
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SETO, Kunisato, Zhixiang XU, Yuuji Yamada, and Liqiang Wang. "On ground liquefaction effect of a ground improvement machine." Proceedings of Conference of Kyushu Branch 2004.57 (2004): 449–50. http://dx.doi.org/10.1299/jsmekyushu.2004.57.449.

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Wang, Yan, Hua Wang, Cunyan Cui, and Beilei Zhao. "Investigating Different Grounds Effects on Shock Wave Propagation Resulting from Near-Ground Explosion." Applied Sciences 9, no. 17 (2019): 3639. http://dx.doi.org/10.3390/app9173639.

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A massive explosion of a liquid-propellant rocket in the course of an accident can lead to a truly catastrophic event, which would threaten the safety of personnel and facilities around the launch site. In order to study the propagation of near-ground shock wave and quantify the enhancement effect on the overpressure, models with different grounds have been established based on an explicit nonlinear dynamic ANSYS/LS-DYNA 970 program. Results show that the existence of the ground will change the propagation law and conform to the reflection law of the shock wave. Rigid ground absorbs no energy
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Plotkin, A., and S. S. Dodbele. "Slender wing in ground effect." AIAA Journal 26, no. 4 (1988): 493–94. http://dx.doi.org/10.2514/3.9920.

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Garcia, Darwin L., and Joseph Katz. "Trapped Vortex in Ground Effect." AIAA Journal 41, no. 4 (2003): 674–78. http://dx.doi.org/10.2514/2.1997.

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LaPierre, Ray. "Hall effect breaks new ground." Nature Nanotechnology 7, no. 11 (2012): 695–96. http://dx.doi.org/10.1038/nnano.2012.191.

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Attenborough, Keith, Imran Bashir, Toby Hill, and Shahram Taherzadeh. "Diffraction assisted rough ground effect." Journal of the Acoustical Society of America 128, no. 4 (2010): 2374. http://dx.doi.org/10.1121/1.3508435.

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Gupta, H., M. Zhang, and A. P. Parakka. "Barkhausen effect in ground steels." Acta Materialia 45, no. 5 (1997): 1917–21. http://dx.doi.org/10.1016/s1359-6454(96)00315-1.

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Wu, J., and N. Zhao. "Ground Effect on Flapping Wing." Procedia Engineering 67 (2013): 295–302. http://dx.doi.org/10.1016/j.proeng.2013.12.029.

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Dissertations / Theses on the topic "Ground effect"

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Read, Gillian Margaret. "Extreme ground effect." Title page, contents and summary only, 1988. http://web4.library.adelaide.edu.au/theses/09PH/09phr284.pdf.

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Cai, Jielong. "Changes in Propeller Performance Due to Ground and Partial Ground Proximity." University of Dayton / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1588164898961792.

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Doig, Graham Mechanical &amp Manufacturing Engineering Faculty of Engineering UNSW. "Compressible ground effect aerodynamics." Awarded by:University of New South Wales. Mechanical & Manufacturing Engineering, 2009. http://handle.unsw.edu.au/1959.4/44696.

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The aerodynamics of bodies in compressible ground effect flowfields from low-subsonic to supersonic Mach numbers have been investigated numerically and experimentally. A study of existing literature indicated that compressible ground effect has been addressed sporadically in various contexts, without being researched in any comprehensive detail. One of the reasons for this is the difficulty involved in performing experiments which accurately simulate the flows in question with regards to ground boundary conditions. To maximise the relevance of the research to appropriate real-world scenarios,
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Purvis, Richard. "Rotor blades and ground effect." Thesis, University College London (University of London), 2002. https://ueaeprints.uea.ac.uk/20790/.

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This thesis uses numerical, asymptotic and flow structural techniques to examine various aspects of rotor blade flows and ground effect. It explores two- and three-dimensional flows, generally concentrating upon regimes that have a degree of relevance to typical rotor blade flows. Chapter 2 considers, as a first step towards understanding a general rotor blade system in ground effect, a finite rotating disc near horizontal ground. More specifically, it concentrates on determining the layer shape beyond the disc rim that, due to the presence of the ground, cannot remain flat without violating a
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Kusmarwanto, I. "Ground effect on a rotor wake." Thesis, Cranfield University, 1985. http://dspace.lib.cranfield.ac.uk/handle/1826/4545.

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The effect of the ground on a rotor wake in forward flight has been investigated experimentally in the working section of an 8ft x Oft straight-through wind tunnel. A three bladed fully articulated rotor with a solidity ratio of 0.07 and diameter of 1.06m, powered by a hydraulic motor, has been tested at a height of 0.47 rotor diameter above a solid ground board which has an elliptical leading edge. Tests have been run at various low advance ratios (<0.1) with two collective pitch settings. A three-element hot wire anemometer probe has been used to measure the average value of the three compon
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Jones, Marvin Alan. "Mechanisms in wing-in-ground effect aerodynamics." Thesis, University College London (University of London), 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.343624.

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An aircraft in low-level flight experiences a large increase in lift and a marked reduction in drag, compared with flight at altitude. This phenomenon is termed the 'wing-in-ground' effect. In these circumstances a region of high pressure is created beneath the aerofoil, and a pressure difference is set up between its upper and lower surfaces. A pressure difference is not permitted at the trailing edge and therefore a mechanism must exist, which allows the pressures above and below to adjust themselves to produce a continuous pressure field in the wake. It is the study of this mechanism and it
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Pulla, Devi Prasad. "A study of helicopter aerodynamics in ground effect." Columbus, Ohio : Ohio State University, 2006. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu1149869712.

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Molina, Juan. "Aerodynamics of an oscillating wing in ground effect." Thesis, University of Southampton, 2011. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.582653.

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This research intends to provide new insight into the aerodynamics of wings in ground effect under dynamic motion. This work represents a new step forward in the field of race car aerodynamics, in which steady aerodynamics are well understood. As the first comprehensive study on oscillating wings in ground effect, several modes of oscillation were studied numerically, including heaving, pitching and combined motion of an airfoil and heaving of a wing fitted with endplates. A wide range of reduced frequencies were tested for the simulations at different ride heights, which showed appreciable di
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Roberts, L. S. "Boundary-layer transition on wings in ground effect." Thesis, Cranfield University, 2017. http://dspace.lib.cranfield.ac.uk/handle/1826/12789.

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The competitiveness of a high-performance racing car is extremely reliant on aerodynamics. Due to the current economic climate, track testing is often forsaken and the majority of aerodynamic development carried out using sub-scale wind tunnel testing and computational simulations. It is important, therefore, that experimental and computational approaches represent real-world conditions as closely as possible. Although racing cars travel at much higher speeds than typical passenger cars, in comparison to aircrafts they still operate at relatively low Reynolds numbers and, consequently, laminar
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Igue, Roberto T. "Experimental Investigation of a lift augmented ground effect platform." Wright-Patterson AFB, OH : Air Force Institute of Technology, 2005. http://handle.dtic.mil/100.2/ADA440437.

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Books on the topic "Ground effect"

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L, Ash Robert, and United States. National Aeronautics and Space Administration., eds. Viscous effects on a vortex wake in ground effect. Old Dominion University Research Foundation, Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University, 1992.

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Curry, Robert E. Ground-effect analysis of a jet transport airplane. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.

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Yun, Liang. WIG craft and ekranoplan: Ground effect craft technology. Springer, 2010.

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Curry, Robert E. Ground-effect analysis of a jet transport airplane. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.

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Curry, Robert E. Ground-effect analysis of a jet transport airplane. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.

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Curry, Robert E. Ground-effect analysis of a jet transport airplane. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.

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H, Bowers Albion, and Dryden Flight Research Facility, eds. Ground-effect analysis of a jet transport airplane. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.

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Wong, J. Y. Theory of ground vehicles. 4th ed. Wiley, 2008.

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Rozhdestvensky, Kirill V. Aerodynamics of a Lifting System in Extreme Ground Effect. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-04240-3.

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Curry, Robert E. Dynamic ground effect for a cranked arrow wing airplane. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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Book chapters on the topic "Ground effect"

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Koketsu, Kazuki. "The Effect of Propagation." In Ground Motion Seismology. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8570-8_3.

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Yun, Liang, Alan Bliault, and Johnny Doo. "Wings in Ground Effect." In WIG Craft and Ekranoplan. Springer US, 2009. http://dx.doi.org/10.1007/978-1-4419-0042-5_1.

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Mendelssohn, Moses, Daniel O. Dahlstrom, and Corey Dyck. "Cause – Effect – Ground – Power." In Studies in German Idealism. Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-94-007-0418-3_2.

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Koketsu, Kazuki. "The Effect of Earthquake Source." In Ground Motion Seismology. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8570-8_2.

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Yoshida, Nozomu. "Effect of Various Factors from Case Studies." In Seismic Ground Response Analysis. Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-94-017-9460-2_15.

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Kleine, H., J. Young, B. Oakes, K. Hiraki, H. Kusano, and Y. Inatani. "Aerodynamic Ground Effect for Transonic Projectiles." In 28th International Symposium on Shock Waves. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-25685-1_78.

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Wang, John G. Z. Q., and K. Tim Law. "Ground waving and its damaging effect." In Siting in earthquake zones. Routledge, 2022. http://dx.doi.org/10.1201/9780203739648-9.

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Dhabu, Anjali, J. Dhanya, and S. T. G. Raghukanth. "Effect of Topography on Earthquake Ground Motions." In Lecture Notes in Civil Engineering. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-0365-4_9.

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Del Cont Bernard, Davide, Mattia Giurato, Fabio Riccardi, and Marco Lovera. "Ground Effect Analysis for a Quadrotor Platform." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-65283-2_19.

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Yun, Liang, and Alan Bliault. "Wings in Ground Effect: Ekranoplans and WIG Craft." In High Performance Marine Vessels. Springer US, 2012. http://dx.doi.org/10.1007/978-1-4614-0869-7_3.

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Conference papers on the topic "Ground effect"

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Tanner, Philip, Luther Jenkins, Austin Overmeyer, Chung-Sheng Yao, and Scott Bartram. "Experimental Investigation of Rotorcraft Outwash in Ground Effect." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10281.

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The wake characteristics of a rotorcraft are affected by the proximity of a rotor to the ground surface, especially during hover. Ground effect is encountered when the rotor disk is within a distance of a few rotor radii above the ground surface and results in an increase in thrust for a given power relative to that same power condition with the rotor out of ground effect. Although this phenomenon has been highly documented and observed since the beginning of the helicopter age, there is still a relatively little amount of flowfield data existing to help understand its features. Joint Army and
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Metry, Aandro, David Peters, and J. V. R. Prasad. "Finite State Modeling of Ground Effect Using Mass Source Distribution at the Ground Plane." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1258.

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Ground effect analytical models in the literature, such as the Pressure Potential Based Finite State Model (PPBFSM) or Velocity Potential Based Finite State Model (VPBFSM) have been developed to study an isolated rotor in full ground effect. These models use the mass source distributions to account for the ground plane. Also, these models consider that the exit pressure of those distributions is equal to the pressure exerted from the rotor at the ground plane. However, PPBFSM and VPBFSM do not satisfy the non-penetration of flow boundary condition at the ground plane. This paper develops a new
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Kherif, O., S. Mousa, S. Robson, et al. "Effect of Ground Rods Position on Current Distribution in Ground Grid under Transient Current." In 2024 59th International Universities Power Engineering Conference (UPEC). IEEE, 2024. https://doi.org/10.1109/upec61344.2024.10892423.

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Cai, Jielong, Sidaard Gunasekaran, Anwar Ahmed, and Michael V. Ol. "Propeller Partial Ground Effect." In AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-1028.

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Coulliette, C., and A. Plotkin. "Airfoil ground effect revisited." In 13th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-1832.

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Thu, May, Ikuo Towhata, and Suguru Yamada. "Laboratory Shear Tests on Effect of Soil Improvement by Fibers." In International Conference on Ground Improvement & Ground Control. Research Publishing Services, 2012. http://dx.doi.org/10.3850/978-981-07-3560-9_03-0301.

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Cherdsak, Suksiripattanapong, and Suksun Horpibulsuk. "Effect of Particle Size on the Pullout Mechanism of Bearing Reinforcement." In International Conference on Ground Improvement & Ground Control. Research Publishing Services, 2012. http://dx.doi.org/10.3850/978-981-07-3560-9_09-0917.

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G. S, Fahmy. "Effect of Geosynthetic base Reinforcement on the Lateral Spreading of Piled-Embankment." In International Conference on Ground Improvement & Ground Control. Research Publishing Services, 2012. http://dx.doi.org/10.3850/978-981-07-3560-9_03-0307.

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Ing, D., and A. Harris. "Ground environment mat (GEM) on ASTOVL ground-effect performance." In International Powered Lift Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-4891.

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Chabalko, Christopher, Timothy Fitzgerald, Marcelo Valdez, and Balakumar Balachandran. "Flapping Aerodynamics and Ground Effect." In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-420.

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Reports on the topic "Ground effect"

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Yokel, Felix Y. Effect of subsurface conditions on earthquake ground motions. National Institute of Standards and Technology, 1993. http://dx.doi.org/10.6028/nist.ir.4769.

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Leonard, Norman J., and III. Wing in Ground Effect Aircraft: An Airlifter of the Future. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada430859.

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Donahue, Jennifer, Jonathan Stewart, Nicolas Gregor, and Yousef Bozorgnia. Ground-Motion Directivity Modeling for Seismic Hazard Applications. Pacific Earthquake Engineering Research Center, University of California, Berkeley, CA, 2019. http://dx.doi.org/10.55461/gphh9609.

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We reviewed five models for modifying the natural log mean and within-event standard deviation of ground-motion models (GMMs) to account for directivity effects in the near-fault environment. We found broad consistency for strike–slip ruptures, with positive and negative directivity effects for cases of rupture towards and away from a site of interest, respectively. We found substantial divergence among directivity models for reverse slip, with some providing maximum directivity for sites positioned to experience the peak alignment of rupture direction with the fault-slip direction (this occur
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Faunt, C. C. Effect of faulting on ground-water movement in the Death Valley region, Nevada and California. Office of Scientific and Technical Information (OSTI), 1997. http://dx.doi.org/10.2172/587919.

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Hammad, Ali, and Mohamed Moustafa. Seismic Behavior of Special Concentric Braced Frames under Short- and Long-Duration Ground Motions. Pacific Earthquake Engineering Research Center, University of California, Berkeley, CA, 2019. http://dx.doi.org/10.55461/zont9308.

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Over the past decade, several long-duration subduction earthquakes took place in different locations around the world, e.g., Chile in 2010, Japan in 2011, China in 2008, and Indonesia in 2004. Recent research has revealed that long-duration, large-magnitude earthquakes may occur along the Cascadia subduction zone of the Pacific Northwest Coast of the U.S. The duration of an earthquake often affects the response of structures. Current seismic design specifications mostly use response spectra to identify the hazard and do not consider duration effects. Thus, a comprehensive understanding of the
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Ismail, Hesham, Eun Joo Lee, KyongYuk Ko, and Dong U. Ahn. Effect of Antioxidant Application Methods on the Color, Lipid Oxidation and Volatiles of Irradiated Ground Beef. Iowa State University, 2009. http://dx.doi.org/10.31274/ans_air-180814-1036.

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Mojidra, Rushil, and Keri Ryan. Influence of Vertical Ground Motion on Bridges Isolated with Spherical Sliding Bearings. Pacific Earthquake Engineering Research Center, University of California, Berkeley, CA, 2019. http://dx.doi.org/10.55461/rynq3624.

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The motivation for this project developed from testing of a full scale building isolated with triple friction pendulum bearings on the E-defense shake table in Japan. The test demonstrated experimentally that the vertical component of ground motion can amplify both the base shear and the story acceleration in the isolated building. Vertical shaking introduced high-frequency variation in the axial force of the bearings, and, consequently, a high-frequency component in the bearing lateral force, which excited higher structural modes in the building. Since vertical bridges are flexible in the ver
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Al-Hijazeen, Marwan, Dong Uk U. Ahn, and Aubrey F. Mendonca. Effect of Oregano Essential Oil on the Storage Stability and Quality Parameters of Ground Chicken Breast Meat. Iowa State University, 2018. http://dx.doi.org/10.31274/ans_air-180814-288.

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Bodie, Mark, Michael Parker, Alexander Stott, and Bruce Elder. Snow-covered obstacles’ effect on vehicle mobility. Engineer Research and Development Center (U.S.), 2020. http://dx.doi.org/10.21079/11681/38839.

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The Mobility in Complex Environments project used unmanned aerial systems (UAS) to identify obstacles and to provide path planning in forward operational locations. The UAS were equipped with remote-sensing devices, such as photogrammetry and lidar, to identify obstacles. The path-planning algorithms incorporated the detected obstacles to then identify the fastest and safest vehicle routes. Future algorithms should incorporate vehicle characteristics as each type of vehicle will perform differently over a given obstacle, resulting in distinctive optimal paths. This study explored the effect of
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Graham Feingold. Investigation of the Aerosol Indirect Effect at the Southern Great Plains Using Ground-Based Remote Sensors and Modeling. Office of Scientific and Technical Information (OSTI), 2006. http://dx.doi.org/10.2172/877271.

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