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2022 | OriginalPaper | Buchkapitel

Nonlinear Aeroelasticity

verfasst von : Earl H. Dowell

Erschienen in: A Modern Course in Aeroelasticity

Verlag: Springer International Publishing

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Abstract

This is an introduction and overview of the work that has been done in nonlinear aeroelasticity prior to the last decade. Many of the issues discussed here are still under active investigation. Of particular interest are the limit cycle oscillations that may occur once the dynamic stability (flutter) boundary has been exceeded.

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Vorheriges Kapitel Experimental Aeroelasticity

Nächstes Kapitel Aeroelastic Control

This chapter is based upon an invited paper prepared by E.H. Dowell, J.W. Edwards and T. Strganac, “Nonlinear Aeroelasticity,” Journal of Aircraft, Vol. 40, No .5, 2003, pp.857–874.

Dowell EH, Edwards JW, Strganac T (2003) Nonlineaeroelasticity. J Aircr 40(5):857–874CrossRef

Thompson JMT, Stewart H (1988) Nonlinear dynamics and chaos. Wiley, New York

Denegri CM Jr (1997) Correlation of classical flutter analyses and nonlinear flutter responses characteristics. International forum on aeroelasticity and structural dynamics, Rome, Italy, June, pp 141–148

Denegri CM Jr, Cutchins MA (1997) Evaluation of classical flutter analysis for the prediction of limit cycle oscillations. AIAA Paper 97–1021

Denegri CM Jr (2000) Limit cycle oscillation flight test results of a fighter with external stores. J Aircr 37(5):761–769CrossRef

Denegri CM Jr, Johnson MR (2001) Limit cycle oscillation prediction using artificial neural networks. J Guid Control Dyn 24(5):887–895CrossRef

AGARD Specialists meeting on wings-with-stores flutter. In: 39th meeting of the structures and materials panel, AGARD Conference proceedings No. 162, Munich, Germany, Oct 1974

Bunton RW, Denegri CM Jr (2000) Limit cycle oscillation characteristics of fighter aircraft. J Aircr 37(5):910–918CrossRef

Cunningham AM Jr (1999) A generic nonlinear aeroelastic method with semi-empirical nonlinear unsteady aerodynamics. Vol 1 and 2, AFRL-VA-WP-R-1999-3014

10.

Cunningham AM Jr (1998) The role of nonlinear aerodynamics in fluid-structure interactions, AIAA Paper 98–2423

11.

Cunningham AM Jr, Geurts EGM (1998) Analysis of limit cycle oscillation/transonic high alpha flow visualization, AFRL-VA-WP-TR-1998-3003, Part I, Jan

12.

Dobbs SK, Miller GD, Stevenson JR (1985) Self induced oscillation wind tunnel test of a variable sweep wing. In: 26th AIAA/ASME/ASCE/AHS structures, Structural dynamics and materials conference. AIAA Paper 85–0739-CP. Orlando, FL, April, pp 15–17

13.

Hartwich PM, Dobbs SK, Arslan AE, Kim SC (2000) Navier-Stokes computations of limit cycle oscillations for a B-1-Like configuration. AIAA Paper 2000–2338, AIAA Fluids 2000. Denver

14.

Dreim DR, Jacobson SB, Britt RT (1999) Simulation of non-linear transonic aeroelastic behavior on the B-2, NASA CP-1999-209136. CEAS/AIAA/ICASE/NASA Langley international forum on aeroelasticity and structural dynamics, pp 511–521

15.

Croft J (2001) Airbus elevator flutter: annoying or dangerous, Aviation week and space technology

16.

Dowell EH (1972) Panel flutter, NASA special publication, SP-8004

17.

Dowell EH (1975) Aeroelasticity of plates and shell. Kluwer academic publishers, New YorkMATH

18.

Yurkovich RN, Liu DD, Chen PC (2001) The state-of-the-art of unsteady aerodynamics for high performance aircraft. AIAA Paper 2001–0428

19.

Dowell EH, Hall KC (2001) Modeling of fluid-structure interaction. Annu Rev Fluid Mech 33:445–490MATHCrossRef

20.

Bennett RM, Edwards JW (1998) An overview of recent developments in computational aeroelasticity. AIAA Paper No. 98–2421, presented at the AIAA fluid dynamics conference, Albuquerque, NM

21.

Beran P, Silva W (2001) Reduced-order modeling: new approaches for computational physics. AIAA Paper 2001–0853, 39th Aerospace sciences meeting and exhibit. Reno

22.

Kim T, Bussoletti JE (2001) An optimal reduced order aeroelastic modeling based on a response - based modal analysis of unsteady CFD models. AIAA Paper 2001–1525

23.

Silva WA (1993) Application of nonlinear systems theory to transonic unsteady aerodynamic responses. J Aircr 30(5):660–668CrossRef

24.

Silva WA (1993) Extension of a nonlinear system theory to general-frequency unsteady transonic aerodynamic responses. In: 34th AIAA structures, structural dynamics, and materials conference. Reston

25.

Silva WA (1993) Extension of a nonlinear systems theory to transonic unsteady aerodynamic responses. AIAA Paper 93–1590

26.

Silva WA (1997) Discrete-time linear and nonlinear aerodynamic impulse responses for efficient (CFD) analyses. Ph.D Thesis, college of William Mary, Williamsburg, Oct

27.

Silva WA (1997) Identification of linear and nonlinear aerodynamic impulse response using digital filter techniques. AIAA atmospheric flight mechanics conference, Reston, VA, pp 584–597

28.

Silva WA (1999) Reduced-order models based on linear and nonlinear aerodynamic impulse response. International forum on aeroelasticity and structural dynamics, NASA Langley research center, Hampton, pp 369–379

29.

Raveh D, Levy Y, Karpel M (2000) Aircraft aeroelastic analysis and design using CFD-based unsteady loads. AIAA Paper 2000–1325, 41st AIAA/ASME/ASCE/AHS/ASC structures, Structural dynamics, and materials conference and exhibit. Atlanta, GA, April

30.

Raveh DE (2001) Reduced-order models for nonlinear unsteady aerodynamics. AIAA J 39(8):1417–1429CrossRef

31.

Farhat C, Geuzaine P, Brown G, Harris C (2002) Nonlinear flutter analysis of an F-16 in stabilized, accelerated, and increased angle of attack flight conditions. AIAA Paper 2002–1490

32.

Farhat C, Harris C, Rixen D (2000) Expanding a flutter envelope using accelerated flight data: application to An F-16 fighter configuration. AIAA Paper 2000–1702

33.

Roughen KM, Baker ML, Fogarty T (2001) Computational fluid dynamics and doublet-lattice calculation of unsteady control surface aerodynamics. J Aircr 24(1):160–166

34.

Schuster DM, Edwards JW, Bennett RM (2000) An overview of unsteady pressure measurements in the transonic dynamics tunnel. AIAA Paper No. 2000–1770, presented at the AIAA dynamics specialists conference, Atlanta

35.

Ashley H (1980) Role of shocks in the ‘Sub-Transonic’ flutter phenomenon. J Aircr 17:187–197

36.

Bartels RE, Schuster DM (2000) A comparison of two navier-stokes aeroelastic methods using BACT Benchmark experimental data. J Guid Control Dyn 23(5):1094–1099CrossRef

37.

Davis SS, Malcolm GN (1980) Transonic shock-wave/boundary layer interactions on an oscillating airfoil. AIAA J 18(11):1306–1312CrossRef

38.

McMullen M, Jameson A, Alonso JJ (2002) Application of a nonlinear frequency domain solver to Euler and Navier-Stokes equations. AIAA Paper 2002–0120. In: 40th AIAA Aerospace sciences meeting and exhibit. Reno

39.

Kreiselmaier E, Laschka B (2000) Small disturbance Euler equations: efficient and accurate tool for unsteady load prediction. J Aircr 37(5):770–778CrossRef

40.

Ruiz-Calavera LP (ed) (2000) Verification and validation data for computational unsteady aerodynamics codes, Research and technology organization TW-26

41.

Farhat C, Lesoinne M (1998) A conservative algorithm for exchanging aerodynamic and elastodynamic data in aeroelastic systems. AIAA Paper 98–0515

42.

Farhat C, Lesoinne M (1998) A higher-order subiteration free staggered algorithm for nonlinear transient aeroelastic problems. AIAA J 36(9):1754–1756CrossRef

43.

Farhat C, Lesoinne M (1998) Enhanced partitioned procedures for solving nonlinear transient aeroelastic problems. AIAA Paper 98–1806

44.

Raveh DE, Levy Y, Karpel M (2001) Efficient aeroelastic analysis using computational unsteady aerodynamics. J Aircr 38(3):547–556CrossRef

45.

Thomas JP, Dowell EH, Hall KC (2001) Nonlinear inviscid aerodynamic effects of transonic divergence, flutter and limit cycle oscillations. In: AIAA Paper 2001–1209, presented at 42nd AIAA/ASME /ASCE /AHS /ASC structures, Structural dynamics and materials conference, Seattle

46.

Thomas JP, Dowell EH, Hall KC (2001) Three-dimensional transonic aeroelasticity using proper orthogonal decomposition based reduced order models. AIAA Paper 2001–1526, presented at 42nd AIAA/ASME /ASCE/AHS /ASC structures, Structural dynamics, and materials conference and exhibit. Seattle, WA, April, pp 16–19

47.

Gupta KK (1996) Development of a finite element aeroelastic analysis capability. J Aircr 33(5):995–1002CrossRef

48.

Scott RC, Silva WA, Florance JR, Keller DF Measurement of unsteady pressure data on a large HSCT semi-span wing and comparison with analysis. AIAA Paper 2002–1648

49.

Silva WA, Keller DF, Florance JR, Cole SR, Scott RC (2000) Experimental steady and unsteady aerodynamic and flutter results for HSCT semi-span models, 41st structures, Structural dynamics and materials conference. AIAA No. 2000–1697, April

50.

Bennett RM, Eckstrom CV, Rivera JA Jr, Danberry BE, Farmer MG, Durham MH (1991) The Benchmark aeroelastic models program: description and highlights of initial results, NASA TM 104180

51.

Bennett RM, Scott RC, Wieseman CD (2000) Computational test cases for the Benchmark active controls model. J Guid Control Dyn 23(5):922–929CrossRef

52.

Ruiz-Calavera LP et al. (1999) A new compendium of unsteady aerodynamic test cases for CFD: summary of AVTWG-003 activities, International forum on aeroelasticity and structural dynamics

53.

Hall KC, Thomas JP, Dowell EH (2000) Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows, AIAA Paper 99–0655. AIAA J 38(10):1853–1862CrossRef

54.

Hall KC, Thomas JP, Dowell EH (1999) Reduced-order modeling of unsteady small disturbance flows using a frequency-domain proper orthogonal decomposition technique. AIAA Paper 99–0655, presented at 37th AIAA Aerospace sciences meeting and exhibition. Reno

55.

Isogai K (1979) On the transonic-dip mechanism of flutter of sweptback wing. AIAA J 17(7):793–795CrossRef

56.

Ehlers FE, Weatherhill WH (1982) A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils, NASA CR-3537

57.

Edwards JW, Bennett RM, Whitlow W Jr, Seidel DA (1983) Time-marching transonic flutter solutions including angle-of-attack effects. J Aircr 20(11):899–906CrossRef

58.

Prananta BB, Hounjet JHL, Zwaan RJ (1998) Two-dimensional transonic aeroelastic analysis using thin-layer Navier-Stokes methods. J Fluids Struct 12:655–676CrossRef

59.

Bohbot J, Darracq D (2001) Time domain analysis of two D.O.F. airfoil flutter using an Euler/turbulent Navier-Stokes implicit solver, International forum on structural dynamics, Vol II, Madrid, Spain, June, pp 75–86

60.

Bendiksen OO (2001) Energy approach to flutter suppression and aeroelastic control. J Guid Control Dyn 24(1):176–184CrossRef

61.

Bendiksen OO (2002) Transonic flutter. In: AIAA Paper 2002–1488, 43rd AIAA/ASME /ASCE/AHS /ASC structures, Structural dynamics and materials conference, Denver, CO, April

62.

Bendiksen OO (2001) Transonic flutter and the nature of the transonic dip, IFASD 2001, Vol 11, Madrid, Spain

63.

Dogget RV Jr, Rainey AG, Morgan HG (1959) An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics, NASA TM X-79

64.

Dowell EH, Crawley EF, Curtiss HC Jr, Peters DA, Scanlan RH, Sisto F (1995) A modern course in aeroelasticity, 3rd edn. Kluwer Academic Publishers, Dordrecht/Boston, p 699MATH

65.

Dowell EH, Tang DM (2002) Nonlinear aeroelasticity and unsteady aerodynamics, AIAA paper 2002–0003. The Theodore von Karman lecture. AIAA J 40(9), 1697–1707

66.

O’ Neil T, Gilliat H, Strganac T (1996) Investigation of aeroelastic response for a system with continuous structural nonlinearities. AIAA Paper 96–1390

67.

Block JJ, Strganac TW (1998) Applied active control for a nonlinear aeroelastic structure. J Guid Control Dyn 21(6):838–845CrossRef

68.

Ko J, Kurdila AJ, Strganac TW (1997) Nonlinear control of a prototypical wing section with torsional nonlinearity. J Guid Control Dyn 20(6):1181–1189MATHCrossRef

69.

Ko J, Strganac TW, Kurdila AJ (1999) Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity. Nonlinear Dyn 18(3):289–301MATHCrossRef

70.

Ko J, Strganac TW, Kurdila AJ (1998) Stability and control of a structurally nonlinear aeroelastic system. J Guid Control Dyn 21(5):718–725CrossRef

71.

Thompson DE, Strganac TW (2000) Store-induced limit cycle oscillations and internal resonance in aeroelastic systems. In: 41st AIAA structures, Structural dynamics and materials conference. AIAA Paper 2000–1413

72.

Cole SR (1990) Effects of spoiler surfaces on the aeroelastic behavior of a low-aspect ratio wing. In: 31st AIAA structures. Structural dynamics and materials conference. AIAA Paper 90–0981:1455–1463

73.

Oh K, Nayfeh AH, Mook DT (1994) Modal interactions in the forced vibration of a cantilever metallic plate. Nonlinear Stoch Dyn 192:237–247

74.

Pai PF, Nayfeh AH (1990) Three-dimensional nonlinear vibrations of composite beams-I: equations of motion. Nonlinear Dyn 1:477–502CrossRef

75.

Stearman RO, Powers EJ, Schwarts J, Yurkorvich R (1991) Aeroelastic system identification of advanced technology aircraft through higher order signal processing. 9th International modal analysis conference. Florence, Italy, April, pp 1607–1616

76.

Gilliatt HC, Strganac TW, Kurdila AJ (1997) Nonlinear aeroelastic response of an airfoil, 35th Aerospace sciences meeting and exhibit. AIAA Paper 97–0459. Reno, pp 258–266

77.

Chang JH, Stearman RO, Choi D, Powers EJ (1985) Identification of aeroelastic phenomenon employing bispectral analysis techniques. Int Modal Anal Conf Exhibit 2:956–964

78.

Tang DM, Dowell EH (2001) Effects of angle of attack on nonlinear flutter of a delta wing. AIAA J 39(1):15–21CrossRef

79.

Gordnier RE, Melville RB (1999) Physical mechanisms for limit-cycle oscillations of a cropped delta wing. AIAA Paper 99–3796, Norfolk

80.

Gordnier RE, Melville RB (2001) Numerical simulation of limit-cycle oscillations of a cropped delta wing using the full Navier-Stokes equations. Int J Comput Fluid Dyn 14(3):211–224MATHCrossRef

81.

Schairer ET, Hand LA (1997) Measurement of unsteady aeroelastic model deformation by stereo photogrammetry. AIAA Paper 97–2217

82.

Preidikman S, Mook DT (2000) Time domain simulations of linear and nonlinear aeroelastic behavior. J Vib Control 6(8):1135–1175CrossRef

83.

Patil MJ, Hodges DH, Cesnik C (1999) Nonlinear aeroelasticity and flight dynamics of highaltitude long-endurance aircraft. AIAA Paper 99–1470

84.

Patil MJ, Hodges DH, Cesnik CE (2000) Nonlinear aeroelastic analysis of complete aircraft in subsonic flow. J Aircr 37(5):753–760CrossRef

85.

Tang DM, Dowell EH (2001) Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings. AIAA J 39(8):1430–1441CrossRef

86.

Kim K, Strganac T (2002) Aeroelastic studies of a cantilever wing with structural and aerodynamic nonlinearities. In: AIAA Paper 2002–1412, 43rd AIAA/ASME/ASCE/AHS/ACS structures, Structural dynamics and materials conference, Denver, CO, April

87.

Crespo da Silva MRM, Glynn CC (1978) Nonlinear flexural-torsional dynamics of inextensional beams-I: equations of motions. J Struct Mech 6(4):437–448CrossRef

88.

Chen PC, Sarhaddi D, Liu DD (1998) Limit cycle oscillation studies of a fighter with external stores. AIAA Paper 98–1727

89.

Kholodar DB, Thomas JP, Dowell EH, Hall KC (2002) A parametric study of transonic airfoil flutter and limit cycle oscillation behavior. In: AIAA Paper 2002–1211, presented at the AIAA/ASME/ASCE/AHS SDM Conference. Denver, CO, April

90.

Knipfer A, Schewe G (1999) Investigations of and oscillation supercritical 2-D wing section in a transonic flow, 36th Aerospace sciences meeting and exhibit. AIAA Paper No. 99–0653

91.

Schewe G, Deyhle H (1996) Experiments on transonic flutter of a two-dimensional supercritical wing with emphasis on the nonlinear effects, proceeding of the royal aeronautical society conference on unsteady aerodynamics, London, UK, July 17–18

92.

Schewe G, Knipfer A, Henke H (1999) Experimentelle und numerisch Untersuchung zum transonischen Flgelflattern im Hinblick auf nichtlineare Effecte, unpublished manuscript

93.

Schewe G, Knipfer A, Mai H, Dietz G (2002) Experimental and numerical investigation of nonlinear effects in transonic flutter, English version (Translated by Dr. W.F. King III), German aerospace center DLR final report number DLR IB 232–2002 J 01, corresponds to final report for BMBF: Nichtlineare Effekte beim transsonischen Flattern (FKZ 13 N 7172), and internal report DLR IB 2001 J03, Accessed 25 Jan 2002

94.

Thomas JP, Dowell EH, Hall KC (2002) Modeling viscous transonic limit cycle oscillation behavior using a harmonic balance approach. AIAA Paper 2002–1414, presented at 43rd AIAA/ASME/ASCE/AHS/ASC structures, Structural dynamics, and materials conference and exhibit. Denver, CO, April, pp 22–25

95.

Weber S, Jones KD, Ekaterinaris JA, Platzer MF (1999) Transonic flutter computations for a 2-D supercritical wing. AIAA Paper 99–0798, 36th Aerospace sciences meeting and exhibit. Reno

96.

Tang L, Bartels RE, Chen PC, Liu DD (2001) Simulation of transonic limit cycle oscillations using a CFD time-marching method. In: AIAA Paper 2001–1290, 42nd AIAA/ASME/ASCE/AHS/ASC structures, Structural dynamics and materials conference, Seattle. WA, April

97.

Castro BM, Ekaterinaris JA, Platzer MF (2002) Navier-Stokes analysis of wind-tunnel interference on transonic airfoil flutter. AIAA J 40(7):1269–1276CrossRef

98.

Thomas JP, Dowell EH, Hall KC (2001) A harmonic balance approach for modeling threedimensional nonlinear unsteady aerodynamics and aeroelasticity, IMECE paper 2003–32532

99.

Edwards JW (1998) Calculated viscous and scale effects on transonic aeroelasticity, AGARDR-822, Numerical unsteady aerodynamic and aeroelastic simulation, Mar, pp. 1-1-1-1

100.

Edwards JW, Schuster DM, Spain CV, Keller DF, Moses RW (2001) MAVRIC Flutter model transonic limit cycle oscillation test. AIAA Paper No. 2001–1291

101.

Edwards JW (1996) Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method, NASA TM-110284

102.

Edwards, J.W., Private communication

103.

Parker EC, Spain CV, Soistmann DL (1991) Aileron Buzz investigated on several generic NASP wing configurations. AIAA Paper 91–0936

104.

Pak C, Baker ML (2001) Control surface buzz analysis of a generic nasp wing. AIAA Paper 2001–1581

105.

Beran PS, Khot NS, Eastep FE, Snyder RD, Zweber JV, Huttsell LJ, Scott JN (2002) The dependence of store-induced limit-cycle oscillation predictions on modeling fidelity, RTO applied vehicle technology panel symposium on reduction of military vehicle acquisition time and cost through advanced modeling and virtual product simulation, Paper \(\#\) 44. France, Paris

106.

Hutsell L, Schuster D, Volk J, Giesing J, Love M (2001) Evaluation of computational aeroelasticity codes for loads and flutter. AIAA Paper 2001–569

107.

Woodson SH (2001) Wing drop, article in the McGraw-Hill 2002 yearbook of science and technology. McGraw-Hill, New York

108.

Chambers JR (1999) Historical review: perspective on experiences with uncommanded lateral motions at high-subsonic and transonic speeds. Ball aerospace & technologies report, Aerospace systems division

109.

Nayfeh AH, Elzebda JM, Mook DT (1989) Analytical study of the subsonic wing-rock phenomenon for slender delta wings. J Aircr 26(9):805–809CrossRef

110.

Ericsson LE (2001) Flow physics generating highly nonlinear lateral stability characteristics of 65-degree delta-wing-body. J Aircr 38(5):932–934CrossRef

111.

Kokolios A, Cook SP (2001) Modeling abrupt wing stall from flight test data, 32nd Annual symposium of the society of flight test engineers. Seattle

112.

Lamar JE, Hall RM, Sanders EN, Cook SP, Grove DV (2003) Status and plans of abrupt wing stall figures-of-merit (FOM) studies from experimental and computational fluid dynamics, NASA technical report in preparation

113.

Heeg J (1993) Analytical and experimental investigation of flutter suppression by piezoelectric actuation, NASA Technical paper 3241

114.

Lazarus KB, Crawley EF, Lin CY (1991) Fundamental mechanism of aeroelastic control with control surface and strain actuation. 32nd AIAA/ASME/ASCE/AHS SDM Conference. Baltimore, MD, April, pp 1817–1831

115.

Lazarus KB, Crawley EF, Lin CY (1997) Multi-variable active lifting surface control using strain actuation: analytical and experimental results. J Aircr 34(3):313–321CrossRef

116.

Vipperman JS, Barker JM, Clark RL, Balas GS (1999) Comparison of \(\mu \)- and H2-synthesis controllers on an experimental typical section. J Guid Control Dyn 22(2):278–285CrossRef

117.

Clark RL, Frampton KD, Dowell EH (2000) Control of a three degree of freedom airfoil with limit cycle behavior. AIAA J Aircr 37(3):533–536CrossRef

118.

Frampton KD, Clark RL (2000) Experiments on control of limit cycle oscillations in a typical section. AIAA J Guid Control Dyn 23(5):956–960CrossRef

119.

Rule JA, Richard RE, Clark RL (2001) Design of an aeroelastic delta wing model for active flutter control. AIAA J Guid Control Dyn 24(5):918–924CrossRef

120.

Richard RW, Rule JA, Clark RL (2001) Genetic spatial optimization of active elements on an aeroelastic delta wing. ASME J Vib Acoust 123:466–471CrossRef

121.

Platanitis G, Strganac T (2002) Control of a wing section with nonlinearities using leading and trailing edge control surfaces. In: AIAA Paper No. 2002–1718, 43rd AIAA/ASME/ASCE/AHS/ACS structures, Structural dynamics and materials conference, Denver, CO, April

Titel: Nonlinear Aeroelasticity
verfasst von: Earl H. Dowell
Verlag: Springer International Publishing
Buch: A Modern Course in Aeroelasticity
Print ISBN: 978-3-030-74235-5

Electronic ISBN: 978-3-030-74236-2

Copyright-Jahr: 2022
DOI: https://doi.org/10.1007/978-3-030-74236-2_11

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