Relevant bibliographies by topics / Delta Wing Aerodynamics

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Delta Wing Aerodynamics'

Author: Grafiati
Published: 4 June 2021
Last updated: 10 February 2022

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Journal articles on the topic "Delta Wing Aerodynamics"

1

Keshav, R. "Aerodynamics of Reverse Delta Wing." International Journal for Research in Applied Science and Engineering Technology 9, no. VI (2021): 3398–403. http://dx.doi.org/10.22214/ijraset.2021.35618.

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Delta wings are mostly used in supersonic jets and fighter aircrafts. A delta wing is naturally stable and produces vortex lift, so the flow separation can be made into increasing lift. This augmented lift comes at an expense of high drag. A reverse delta wing is nothing but an inverted delta wing, the forward swept wings were inspired from this design. It has low drag coefficient and was used in ground effect vehicle. This paper aims to bring out all the possible studies and research work done on a reverse delta wing. The study was mainly inspired by the works of Alexander Lippisch and his de
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Gursul, I. "Recent developments in delta wing aerodynamics." Aeronautical Journal 108, no. 1087 (2004): 437–52. http://dx.doi.org/10.1017/s0001924000000269.

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Abstract Recent developments in delta wing aerodynamics are reviewed. For slender delta wings, recent investigations shed more light on the unsteady aspects of shear-layer structure, vortex core, breakdown and its instabilities. For nonslender delta wings, substantial differences in the structure of vortical flow and breakdown may exist. Vortex interactions are generic to both slender and nonslender wings. Various unsteady flow phenomena may cause buffeting of wings and fins, however, vortex breakdown, vortex shedding, and shear layer reattachment are the most dominant sources. Dynamic respons
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Viswanath, P. R., and S. R. Patil. "Aerodynamic characteristics of delta wing–body combinations at high angles of attack." Aeronautical Journal 98, no. 975 (1994): 159–70. http://dx.doi.org/10.1017/s0001924000049848.

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AbstractAn experimental study investigating the aerodynamic characteristics of generic delta wing-body combinations up to high angles of attack was carried out at a subsonic Mach number. Three delta wings having sharp leading edges and sweep angles of 50°, 60° and 70° were tested with two forebody configurations providing a variation of the nose fineness ratio. Measurements made included six-component forces and moments, limited static pressures on the wing lee-side and surface flow visualisation studies. The results showed symmetric flow features up to an incidence of about 25°, beyond which
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Muir, Rowan Eveline, Abel Arredondo-Galeana, and Ignazio Maria Viola. "The leading-edge vortex of swift wing-shaped delta wings." Royal Society Open Science 4, no. 8 (2017): 170077. http://dx.doi.org/10.1098/rsos.170077.

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Recent investigations on the aerodynamics of natural fliers have illuminated the significance of the leading-edge vortex (LEV) for lift generation in a variety of flight conditions. A well-documented example of an LEV is that generated by aircraft with highly swept, delta-shaped wings. While the wing aerodynamics of a manoeuvring aircraft, a bird gliding and a bird in flapping flight vary significantly, it is believed that this existing knowledge can serve to add understanding to the complex aerodynamics of natural fliers. In this investigation, a model non-slender delta-shaped wing with a sha
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Wang, Jinjun, and Yan Xu. "Experimental Studies on Control of Delta Wing Aerodynamics." AIAA Journal 42, no. 2 (2004): 403–5. http://dx.doi.org/10.2514/1.9101.

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Traub, Lance W., Brian Moeller, and Othon Rediniotis. "Low-Reynolds-Number Effects on Delta-Wing Aerodynamics." Journal of Aircraft 35, no. 4 (1998): 653–56. http://dx.doi.org/10.2514/2.2352.

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Grismer, Deborah S., Robert C. Nelson, and Wayne L. Ely. "Influence of sideslip on double delta wing aerodynamics." Journal of Aircraft 32, no. 2 (1995): 451–53. http://dx.doi.org/10.2514/3.46740.

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Mochizuki, Saya, and Gouji Yamada. "Aerodynamic characteristics and flow field of delta wings with the canard." MATEC Web of Conferences 145 (2018): 03010. http://dx.doi.org/10.1051/matecconf/201814503010.

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Now, many kinds of explorations for outer planets have been proposed around the world. Among them Mars attracts much attention for future exploration. Orbiters and landers have been used for Mars exploration. Recently as a new exploration method, the usage of an airplane has been seriously considered and there are some development projects for Mars airplane. However, the airplane flying on the Earth atmosphere cannot fly on the Mars atmosphere, because atmospheric conditions are much different each other. Therefore, we focused on the usage of the airplane with unfolding wings for Mars explorat
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9

SHI, ZHIWEI, and XIAO MING. "EXPERIMENTAL INVESTIGATION ON A PITCHING MOTION DELTA WING IN UNSTEADY FREE STREAM." Modern Physics Letters B 23, no. 03 (2009): 409–12. http://dx.doi.org/10.1142/s0217984909018527.

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As combat aircraft becomes more and more maneuverable, the need to understand the unsteady behavior of aircraft in dynamic flow fields becomes more important. Usually researchers pay more attention to the effects on the changes of AOA, but ignore the effects of velocity variations. It is known that the velocity of aircraft changes greatly when the aircraft undergoes a high angle of attack maneuver, like "cobra" maneuver. To completely simulate and study the effect of rapid changes in both free stream velocity and angle of attack, a pitching motion setup is developed in the unsteady wind tunnel
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Maria Viola, Ignazio, and Richard G. J. Flay. "Sail Aerodynamics: On-Water Pressure Measurements on a Downwind Sail." Journal of Ship Research 56, no. 04 (2012): 197–206. http://dx.doi.org/10.5957/jsr.2012.56.4.197.

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Pressures on three horizontal sections of a downwind sail were measured for several wind directions and sail trims. The pressure distributions were compared with wind tunnel tests; similarities and differences were found, the latter as a result of the dynamic effects, which were not modeled in the wind tunnel. A pressure distribution at the head of the spinnaker resembling that from a delta wing was measured at an apparent wind angle of 120°.
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Dissertations / Theses on the topic "Delta Wing Aerodynamics"

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Vaughan, Jon. "Motion induced aerodynamics of a pitching delta wing." Thesis, University of Bath, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.338376.

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Current trends in modem combat aircraft design have seen a move towards canard configurations with all moving foreplanes, providing a manoeuvre advantage with reduced stability. At the same time, with rapid advances in the field of assisted flight control and emphasis now placed on computer controlled, fly-by-wire aircraft, there is an unprecedented requirement for detailed knowledge of motion dependent aerodynamics, such as may be experienced on a foreplane undergoing rapid corrective motions. In this study, investigations have been carried out into the rigid body, motion dependent aerodynami
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2

Allan, Mark. "A CFD investigation of wind tunnel interference on delta wing aerodynamics." Thesis, University of Glasgow, 2002. http://theses.gla.ac.uk/4081/.

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To explore the influence of wind tunnel test facilities on delta wing aerodynamics, the interference has been separated into two distinct types, wall interference and support structure interference. The wall interference effects have been split into three further components, tunnel blockage, side wall interference, and roof and floor interference. Splitting the tunnel influence in this way allows us to determine the most detrimental interference effects, thus allowing the wind tunnel engineer to design experiments accordingly. Euler and more realistic RANS simulations of tunnel interference ha
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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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Le, Moigne Yann. "Adaptive Mesh Refinement and Simulations of Unsteady Delta-Wing Aerodynamics." Doctoral thesis, KTH, Aeronautical and Vehicle Engineering, 2004. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-3786.

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<p>This thesis deals with Computational Fluid Dynamics (CFD)simulations of the flow around delta wings at high angles ofattack. These triangular wings, mainly used in militaryaircraft designs, experience the formation of two vortices ontheir lee-side at large angles of attack. The simulation ofthis vortical flow by solving the Navier-Stokes equations isthe subject of this thesis. The purpose of the work is toimprove the understanding of this flow and contribute to thedesign of such a wing by developing methods that enable moreaccurate and efficient CFD simulations.</p><p>Simulations of the for
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Görtz, Stefan. "Realistic simulations of delta wing aerodynamics using novel CFD methods." Doctoral thesis, KTH, Aeronautical and Vehicle Engineering, 2005. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-125.

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<p>The overall goal of the research presented in this thesis is to extend the physical understanding of the unsteady external aerodynamics associated with highly maneuverable delta-wing aircraft by using and developing novel, more efficient computational fluid dynamics (CFD) tools. More specific, the main purpose is to simulate and better understand the basic fluid phenomena, such as vortex breakdown, that limit the performance of delta-wing aircraft. The problem is approached by going from the most simple aircraft configuration - a pure delta wing - to more complex configurations. As the flow
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Görtz, Stefan. "Realistic simulations of delta wing aerodynamics using novel CFD methods /." Stockholm, 2005. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-125.

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Trussa, Colin Weidner. "Low-Speed Aerodynamic Characteristics of a Delta Wing with Deflected Wing Tips." The Ohio State University, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1586450691890636.

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Williams, Nathan M. "Active flow control on a nonslender delta wing." Thesis, University of Bath, 2009. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.501373.

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The effects of active flow control by oscillatory blowing at the leading edge of a nonslender delta wing with a Λ=50° sweep angle have been investigated. Pressure measurements and Particle Image Velocimetry measurements were conducted on a half wing to investigate the formation of leading edge vortices for oscillatory blowing, compared to the stalled flow for the no blowing case. Stall has been delayed by up to 8, and significant increases in the upper surface suction force have been observed. Velocity measurements show that shear layer reattachment is promoted with forcing, and a vortex flow
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Jupp, Martyn Leonard Edward. "A statistical approach to the analysis of surface pressure measurements on a pitching delta wing." Thesis, University of Glasgow, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.341739.

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Hubner, James Paul. "An investigation of quasiperiodic structures in the vortical flow over Delta wing configuration." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/12243.

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Books on the topic "Delta Wing Aerodynamics"

1

Wood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. Langley Research Center, 1987.

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2

Lee, Elizabeth M. Conical Euler solution for a highly-swept delta wing undergoing wing-rock motion. National Aeronautics and Space Administration, Langley Research Center, 1990.

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Wood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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4

Thompson, Scott A. Surface pressure distributions on a delta wing undergoing large amplitude pitching oscillations. Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1990.

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5

Covell, Peter F. Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds. Langley Research Center, 1987.

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6

Craig, Ken. Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings. Stanford University, Dept. of Aeronautics and Astronautics, 1991.

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Craig, Ken. Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings. Stanford University, Dept. of Aeronautics and Astronautics, 1991.

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8

Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.

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Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.

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Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.

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Book chapters on the topic "Delta Wing Aerodynamics"

1

Hirschel, Ernst Heinrich, Arthur Rizzi, Christian Breitsamter, and Werner Staudacher. "Small Aspect-Ratio Delta-Type Wing Flow." In Separated and Vortical Flow in Aircraft Wing Aerodynamics. Springer Berlin Heidelberg, 2020. http://dx.doi.org/10.1007/978-3-662-61328-3_10.

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Hirschel, Ernst Heinrich, Arthur Rizzi, Christian Breitsamter, and Werner Staudacher. "Selected Flow Problems of Small Aspect-Ratio Delta-Type Wings." In Separated and Vortical Flow in Aircraft Wing Aerodynamics. Springer Berlin Heidelberg, 2020. http://dx.doi.org/10.1007/978-3-662-61328-3_11.

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3

Nakamura, Y., Y. Nakajima, and W. Jia. "Aerodynamic Characteristics of Thick Delta Wing." In Fluid Dynamics of High Angle of Attack. Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-52460-8_26.

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Schütte, Andreas, and Rebeca Nunes Marini. "Computational Aerodynamic Sensitivity Studies for Generic Delta Wing Planforms." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-25253-3_33.

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5

Wiemer, P., K. Haag, and J. Ballmann. "Approximation of Free and Bounded Vortex Sheets at Delta-Wings." In Panel Methods in Fluid Mechanics with Emphasis on Aerodynamics. Vieweg+Teubner Verlag, 1988. http://dx.doi.org/10.1007/978-3-663-13997-3_22.

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Sato, J., K. Fujii, D. Umezawa, and Y. Sunada. "Experimental Aerodynamics on Rolling Delta Wings at High Angles of Attack." In Fluid Dynamics of High Angle of Attack. Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-52460-8_30.

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McCormick, B. W. "Aerodynamics of Delta Wings with Application to High- Alpha Flight Mechanics." In Orbital Transport. Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-45720-3_23.

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Möhlenkamp, K., and E. Fegel. "Real Time for the Calculation of the Aerodynamic of Aircrafts with Delta Wings." In Orbital Transport. Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-45720-3_27.

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Allegre, J., X. Heriard Dubreuilh, and M. Raffin. "TEST CASE VTI-5 Aerodynamic Forces Applied to a Delta Wing Located in Rarefied Hypersonic Flows." In Hypersonic Flows for Reentry Problems. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-77922-0_61.

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Rault, Didier F. G. "Aerodynamic Performance of Delta Wings in The Hypersonic Rarefied Flow Regime. Comparison of 3D Dsmc Simulation With Wind Tunnel Data." In Hypersonic Flows for Reentry Problems. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-77922-0_72.

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Conference papers on the topic "Delta Wing Aerodynamics"

1

NG, T., GERALD MALCOLM, and LIANE LEWIS. "Flow visualization study of delta wings in wing-rock motion." In 7th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2187.

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BUCHHOLZ, MARK, and JIN TSO. "Vortex trapping on a 60 degree delta wing." In 10th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2639.

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NG, T., TONY SKAFF, and JOHN KOUNTZ. "Effect of leeward flow dividers on the wing rock of a delta wing." In 11th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3492.

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Lee, Shiang-yu. "An Analytical Representation of Delta Wing Aerodynamics." In 4th AIAA Theoretical Fluid Mechanics Meeting. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-5192.

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LeRoy, Jean-Francois, Ivan Mary, and Ovide Rodriguez. "CFD Solutions of 70-deg Delta Wing Flows." In 21st AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-4219.

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LEMAY, S., S. BATILL, and R. NELSON. "Leading edge vortex dynamics on a pitching delta wing." In 6th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2559.

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SIRBAUGH, JAMES. "Euler analysis of the AFWAL 65-deg delta wing." In 5th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2272.

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Allan, Mark, Ken Badcock, G. Barakos, and B. Richards. "A RANS Investigation of Wind Tunnel Interference Effects on Delta Wing Aerodynamics." In 21st AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-4214.

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Vardaki, Eleni, and Ismet Gursul. "Vortex Flows on a Rolling Nonslender Delta Wing." In 22nd Applied Aerodynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-4729.

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Greenblatt, David, Yousef Kastantin, Navid Nayeri, and Oliver Paschereit. "Delta Wing Flow Control Using Dielectric Barrier Discharge Actuators." In 25th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-4277.

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