Research into vortex breakdown control

Werlé H. Quelques résultats expérimentaux sur les ailes en flèche, aux faibles vitesses, obtenus en tunnel hydrodynamique. La Recherche Aéronautique, No 41, Septembre–Octobre, 1954. Benjamin, 1967, Some developments in the theory of vortex breakdown, J Fluid Mech, Part 1, 28, 65, 10.1017/S0022112067001909 Sarpkaya, 1971, On stationary and traveling vortex breakdowns, J Fluid Mech, Part 3, 45, 545, 10.1017/S0022112071000181 Délery, 1994, Aspects of vortex breakdown, Progr Aerospace Sci, 30, 1, 10.1016/0376-0421(94)90002-7 Werlé H, Sur l’éclatement des tourbillons d’apex d’une aile delta aux faibles vitesses. La Recherche Aéronautique No. 74, Janvier–Février, 1960. Délery, 2001, Robert legendre, Henri Werlé, Ann Rev Fluid Mech, 33, 129, 10.1146/annurev.fluid.33.1.129 Ringleb FO. Separation control by trapped vortices. Boundary layer and flow control, vol. 1. Pergamon Press, New York, 1961, p. 265–94. Behrbohn H. Basic low-speed aerodynamics of the short-coupled canard configuration of small aspect ratio. SAAB, Sweden, TN-60, July 1965. Smith CW, Ralston JN, Mann HW. Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience. Summary and Analysis NASA CR-3053, Vol. 1, July 1979. Lamar, 1980, Analysis and design of strake-wing configuration, J Aircraft, 17, 20, 10.2514/3.57870 Frink, 1981, Analysis of strake vortex breakdown characteristics in relation to design features, J Aircraft, 18, 252, 10.2514/3.57489 Rao DM. Leading-edge vortex flap experiments on a 74° delta wing. NASA CR 159161, 1979. Rao DM. Leading-edge ‘Vortex Flaps’ for enhanced subsonic aerodynamics of slender wings, 12th Congress of the ICAS, ICAS Proceedings, Munich, Germany, ICAS-80-13.5, October 1980, p. 554–62. Marchman III, 1981, Effectiveness of leading-edge vortex flaps on 60 and 70 degree delta wings, J Aircraft, 18, 280, 10.2514/3.44702 Marchman III JF. The aerodynamics of inverted leading-edge flaps on delta wings. 19th AIAA Aerospace Sciences Meeting, St. Louis, MI, AIAA-81-0365, January 1981. Marchman III JF. Grantz AC. Trailing edge flap influences on leading edge vortex flap aerodynamics. 20th AIAA Aerospace Sciences Meeting, Orlando, FL, AIAA-82-0128, January 1982. Marchman III JF, Terry JE. The impact of strakes on a vortex-flapped delta wing. AIAA Applied Aerodynamics Conference, Danvers, MA, AIAA-83-1814, July 1983. Rao DM, Buter TA. Experimental and computations studies of a delta wing apex-flap. AIAA Applied Aerodynamics Conference, Danvers, MA, AIAA-83-1815, July 1983. Klute SM, Rediniotis OK, Telionis DP. Flow control over delta wings at high angles of attack. 11th AIAA Applied Aerodynamics Conference, AIAA-93-3494, August 1993. Hoffler KD, Rao DM. Investigation of the “Tabbed” vortex flap. Second AIAA Applied Aerodynamics Conference, Seattle, WA, AIAA-83-1812, 1984. Wahls, 1986, Experimental investigation of apex fence flaps on delta wings, J Aircraft, 23, 789, 10.2514/3.45382 Schaeffer NW, Rediniotis OK, Telionis DP. Controlling of delta wing leading-edge vortex with cavity flaps. ASME Flow, Acoustics, Interaction and Fluid Flow Control Symposium of the 1993 Winter Annual Meeting, ASME Paper 93-WA/NCA-27, November 1993. Schaeffer NW, Rediniotis OK, Telionis DP. Control of transient development of leading-edge vortices by vortex cavity flaps. 25th AIAA Fluid Dynamics Conference, Colorado Springs, CO, AIAA-94-1857, June 1994. Hebbar, 1994, Experimental study of vortex flow control on double-delta wings using fillets, J Aircraft, 33, 743, 10.2514/3.47010 Pilkington DJ, Wood NJ. Unsteady aerodynamic effects of trailing edge controls on delta wings. 19th Congress of the International Council of the Aeronautical Sciences, Anaheim, CA, ICAS-94-10-1.1, September 1994. Gursul I, Yang H, Deng Q. Control of vortex breakdown with leading-edge devices. 33rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-95-0676, January 1995. Gursul, 1995, Active control of vortex breakdown over a delta wing, AIAA J, 33, 1743, 10.2514/3.12721 Rao DM, Sharma G, Telionis D. Active control of vortex lift at high angles of attack. 33rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA 95-0653, January 1995. Vorobieff, 1996, Multiple-actuator control of vortex breakdown on a pitching delta wing, AIAA J, 34, 2184, 10.2514/3.13369 Deng, 1996, Effect of leading-edge flaps on vortices and vortex breakdown, J Aircraft, 33, 1079, 10.2514/3.47060 Lambourne NC, Bryer DW. The bursting of leading-edge vortices-some observations and discussion of the phenomenon. ARC, R&M No. 3282 (22775), 1961. Hummel, 1967, Zur umstronmung scharfkantiger schlanker deltaflugel bei grossen anstellwinkeln, Z. Flugwiss, 15, 376 Dixon CJ. Lift augmentation by lateral blowing over a lifting surface. AIAA/AHS VTOL Research, Design, and Operations Meeting, Atlanta, GA, AIAA-69-193, February 1969. Cornish III JJ. High lift applications of spanwise blowing. 7th Congress of the International Council of the Aeronautical Sciences, ICAS Paper No. 70-09, Rome, Italy, September 1970. Cornish III JJ. Vortex flows. AIAA Applied Aerodynamics Conference, Danvers, MA, AIAA-83-1812, July 1983. Parmenter, 1990, Transient response of leading-edge vortices to localized suction, AIAA J, 28, 1131, 10.2514/3.25177 Owens DB, Perkins J. Vortex suppression on highly-swept wings by suction boundary-layer control. 33rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-95-0683, January 1995. McCormick, 1996, Effect of shear-layer control on leading-edge vortices, J Aircraft, 33, 1087, 10.2514/3.47061 Maines BH, Moeller B, Rediniotis OK. The effects of leading-edge suction on delta wing vortex breakdown. 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-99-0128, January 11–14, 1999. Legendre R. Etude théorique du soufflage près du bord de fuite d’un profil d’aile. ONERA Note Technique No. 12/1308A, Avril 1954. Werlé H, Fiant C. Visualisation hydrodynamique de l’écoulement à basse vitesse autour d’une maquette d’avion du type ‘Concorde’. La Recherche Aérospatiale No. 102, 1964. Helin, 1994, Effects of trailing-edge jet entrainment on delta wing vortices, AIAA J, 32, 802, 10.2514/3.12056 Nawrocki D. Differential and vectored trailing-edge jet control of delta wing vortices. 33rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-95-0008, January 1995. Shih, 1996, Trailing-edge jet control of leading edge vortices of a delta wing, AIAA J, 34, 1447, 10.2514/3.13252 Vorobieff, 1996, Multiple-actuator control of vortex breakdown on a pitching delta wing, AIAA J, 34, 2184, 10.2514/3.13369 Vorobieff, 1998, Vortex breakdown on pitching delta wing, AIAA J, 36, 585, 10.2514/2.409 Mitchell AM, Molton P, Barberis D, Délery J. Control of leading-edge vortex breakdown by trailing-edge injection. 17th AIAA Applied Aerodynamics Conference, Norfolk, VA, AIAA-99-3202, June–July 1999. Alexander AJ. Experiments on a delta wing using leading-edge blowing to remove secondary separation. Aeronautical Research Council 24996, May 1963. Trebble WJG. Exploratory investigation of the effects of blowing from the leading-edge of a delta wing. RAE Technical Report No. 66125, ARC 28391, 1966. Dixon CJ. Lift augmentation by lateral blowing over a lifting surface. AIAA/AHS VTOL Research, Design, and Operations Meeting, Atlanta, GA, AIAA-69-193, February 1969. Cornish III JJ. High lift applications of spanwise blowing. Proceedings of the Seventh Congress of the International Council of the Aeronautical Sciences, ICAS Paper No. 70-09, Rome, Italy, September 1970. Poisson-Quinton Ph. Contrôle du décollement d’une surface portante par un jet transversal. Intervention au Congrès ICAS, Rome, Septembre 1970. Werlé H. Sur l’éclatement des tourbillons. ONERA Note Technique No. 175, 1971. Spillman J, Goodridge M. Flow characteristics about a delta wing at 15° incidence with and without edge blowing. Cranfield Report Aero. No. 9, April 1972. Bradley, 1974, A conceptual study of leading-edge-vortex enhancement by blowing, J Aircraft, 11, 33, 10.2514/3.60318 Bradley, 1976, Leading-edge vortex augmentation in compressible flow, J Aircraft, 13, 238, 10.2514/3.58652 Campbell, 1976, Augmentation of vortex lift by spanwise blowing, J Aircraft, 13, 727, 10.2514/3.58703 Dixon CJ, Dansby T, Poisson-Quinton P. Benefits of spanwise blowing at transonic speeds. 11th International Congress of Aeronautical Sciences (ICAS), Lisbon, Portugal, September 1978. Erickson GE. Effects of spanwise blowing on the aerodynamic characteristics of the F-5E. 17th AIAA Aerospace Sciences Meeting, AIAA-78-118, January 1979. Seginer A, Salomon M. Augmentation of fighter aircraft performance by spanwise blowing over the wing leading edge. NASA-TM-84330, March 1983. Er-El J, Seginer A. Effects of spanwise blowing on pressure distribution and leading-edge vortex stability. 15th Congress of the International Council of the Aeronautical Sciences, London, ICAS-86-2.5.1, September 1986. Satran DR, Gilbert WP, Anglin EL. Low-speed stability and control wind tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack. NASA TP-2431, May 1985. Anglin E, Satran D. Effects of spanwise blowing on two fighter configurations. AIAA Atmospheric Flight Mechanics Conference for Future Space Systems, Boulder, CO, AIAA-79-1663, August 1979. Owen FK, Peake DJ. Vortex breakdown and control experiments in the Ames-Dryden water tunnel. Fluid Dynamics Panel Symposium on Aero and Related Hydrodynamic Studies Using Water Facilities, Monterey, CA, October 1986. Shi Z, Wu JM, Vakili AD. An investigation of leading-edge vortices on delta wings with jet blowing. 25th AIAA Aerospace Sciences Meeting, Reno, NV, AIAA-87-0330, January 1987. Visser KD, Iwanski KP, Nelson RC, Ng TT. Control of leading edge vortex breakdown by blowing. 26th AIAA Aerospace Sciences Meeting, Reno, NV, AIAA 88-0504, January 1988. Wood, 1988, Control of vortical lift on delta wings by tangential leading-edge blowing, J Aircraft, 25, 236, 10.2514/3.45583 Wood NJ, Lee KT, Roberts L. Dynamic control of vortical flow on delta wings at high angles of attack. AIAA Atmospheric Flight Mechanics Conference, Minneapolis, MN, AIAA-88-4333, August 1988. Iwanski K, Ng TT, Nelson RC. An experimental investigation of delta wing vortex flow with and without external jet blowing. 27th AIAA Aerospace Sciences Meeting, Reno, NV, AIAA-89-0084, January 1989. Reynolds G, Abtahi A. Three-dimensional vortex development, breakdown and control. Second AIAA Shear Flow Conference, Tempe, AZ, AIAA-89-0998, March 1989. Roberts L, Wood NJ. Control of vortex aerodynamics at high angles of attack. AGARD FDP, Paper No 12, Madrid, Spain, 2–5 October 1989. Pagan D, Molton P, Solignac JL. Etude expérimentale et simulation numérique de l’éclatement d’un tourbillon d’ailettes. ONERA Rapport Technique No. 38/1147 AY, Septembre 1988. Pagan D. Contribution à l’étude expérimentale et théorique de l’éclatement tourbillonnaire en air incompressible. ONERA Note Technique 1990-12, 1990. Pagan D. Molton P. Etudes fondamentales sur l’éclatement tourbillonnaire et son contrôle. Vortex Flow Aerodynamics, AGARD CP-494, Paper 23, Octobre 1990. Afchain D, Deluc JM. Etude des nappes tourbillonnaires sur une aile delta de 70 degrés de flèche a 27 degrés d’incidence. Contrôle de l’éclatement par soufflage. Soufflerie F2. ONERA Rapport Technique No 54/1147 ANG, Septembre 1992. Laval-Jeantet R. Contribution a l’étude du contrôle actif de l’éclatement incompressible. Thèse de Doctorat, Université d’Aix-Marseille II, Marseille, France, 30 Mars 1993. Miller S, Gile B. The effects of blowing on delta wing vortices during dynamic pitching at high angles of attack. 30th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-92-0407, January 1992. Johari, 1996, Delta wing vortex manipulation using pulsed and steady blowing during ramp-pitching, J Aircraft, 33, 452, 10.2514/3.46938 Hong, 1996, Effects of leading-edge lateral blowing on delta wing aerodynamics, AIAA J, 34, 2471, 10.2514/3.13426 Kuo, 1997, Evolution of vortical structure over delta wing with transient along-core blowing, AIAA J, 35, 617, 10.2514/2.181 Kuo, 1998, Unsteady vortex structure over delta-wing subject to transient along core blowing, AIAA J, 36, 1658, 10.2514/2.568 Faler, 1977, Disrupted states of vortex flow and vortex breakdown, Phys Fluids, 2, 1385, 10.1063/1.862033 Guillot S, Gutmark EJ, Garrison TJ. Delay of vortex breakdown over a delta wing via near-core blowing. 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 98-0315, January 1998. Mitchell, 2000, Oscillation of vortex breakdown location and control of the time-averaged location by blowing, AIAA J, 33, 793, 10.2514/2.1059 Mitchell AM, Molton P, Barberis D, Délery J. Control of vortex breakdown location by symmetric and asymmetric blowing. 30th AIAA Fluid Dynamics Conference, Norfolk, VA, AIAA 99-3652, 28 June–1 July 1999. Mitchell AM, Molton P, Barberis D, Gobert J-L. Control of vortex breakdown by along-the-core blowing. AIAA Fluids 2000 Conference, Denver, CO, AIAA-00-2608, June 2000. Mitchell AM. Caractérisation et contrôle de l’éclatement tourbillonnaire sur une aile delta aux hautes incidences. Thèse de Doctorat, Université de Paris 6, Departement de Mécanique, Juillet 2000. Gad-El-Hak, 1987, Control of the discrete vortices from a delta wind, AIAA J, 25, 1042, 10.2514/3.9740 Magness C, Robinson O, Rockwell D. Control of leading edge vortices on a delta wing. Second AIAA Shear Flow Conference, Tempe, AZ, AIAA-89-0999, March 1989. Gu, 1993, Control of vortices on a delta wing by leading-edge injection, AIAA J, 31, 1177, 10.2514/3.11749 Guy Y, Morrow JA, McLaughlin TE. Control of vortex breakdown on a delta wing by periodic blowing and suction. 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-99-0132, January 1999. Guy Y, Morrow JA, McLaughlin TE. Pressure measurements and flow field visualization on a delta wing with periodic blowing and suction. AIAA Atmospheric Flight Mechanics Conference and Exhibit, Portland, OR, AIAA-99-4178, August 1999. Guy Y, Morrow JA, McLaughlin TE, Wygnanski I. Velocity measurements on a delta wing with periodic blowing and suction. 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-2000-0550, January 2000. Guy Y, Morrow JA, McLaughlin TE, Wygnanski I. Parametric investigation of the effects of active flow control on the normal force of a delta wing. 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-2000-0549, January 2000. Morton SA, Guy Y, Morrow JA, Blake DC. Numerical simulation of periodic suction and blowing control of vortex breakdown on a delta wing. 17th AIAA Applied Aerodynamics Conference, Norfolk, VA, AIAA-99-3195, June 1999. Jupp ML, Coton FN, Green RB, Galbraith RA. An analysis of a pitching delta wing using high resolution pressure measurements. 16th AIAA Applied Aerodynamics Conference, Albuquerque, NM, AIAA-98-2743, June 1998. Jupp ML, Coton FN, Green RB. An analysis of high resolution pressure signals on a pitching delta wing. 17th AIAA Applied Aerodynamics Conference, Norfolk, VA, AIAA-99-3111, June 1999.