Accardo, L., Cenedese, A. & Cioffi, F.
1984
Experimental analysis of tip vortex by laser Doppler anemometry.
2nd Int Symp. on Applications of Laser Anemometry to Fluid Mechanics, Lisbon Portugal, July 2–5.
Antonia, R. A. & Britz, D.
1989
Phase-averaging in the turbulent far wake.
Exps. Fluids
7,
138–142.
Baker, G. R., Barker, S. J., Bofah, K. K. & Saffman, P. G.
1974
Laser anemometer measurements of trailing vortices in water.
J. Fluid Mech.
65,
325–336.
Baldwin, B. S., Chigier, N. A. & Sheaffer, Y. S.
1973
Decay of far-flowfield in trailing vortices.
AIAA J.
11,
1601–1602.
Bandyopadhyay, P. R., Stead, D. J. & Ash, R. L.
1991
Organized nature of a turbulent trailing vortex.
AIAA J.
29,
1627–1633.
Batchelor, G. K.
1964
Axial flow in trailing line vortices.
J. Fluid Mech.
12,
645–658.
Bechner, W.
1975
Inequalities in Fourier Analysis.
Annl Maths
102,
159–182.
Betz, A.
1933
Behavior of vortex systems.
NACA Tech. Note 713, pp.
237–253.
Bilanin, A. J., Teske, M. E. & Williamson, G. G.
1977
Vortex interactions and decay in aircraft wakes.
AIAA J.
15,
250–260.
Bisgood, P. L., Maltby, R. L. & Dee, F. W.
1971
Some work at the Royal Aircraft Establishment on the behavior of vortex wakes. In
Aircraft Wake Turbulence and its Detection (ed.J. H. Olsen, A. Goldberg & M. Rogers), pp.
171–206.
Plenum.
Brandt, S. A. & Iversen, J. D.
1977
Merging of aircraft trailing vortices.
J. Aircraft
14,
1212–1220.
Browne, L. B. W., Antonia, R. A. & Chua, L. P.
1989
Calibration of X-probes for turbulent flow measurement.
Exps. Fluids
7,
201–208.
Chigier, N. A. & Corsiglia, V. R.
1971
Tip vortices – velocity distributions.
NASA TM-62,087.
Choi, K. & Simpson, R. L.
1987
Some mean-velocity, turbulence and unsteadiness characteristics of the VPI Stability Wind Tunnel.
Rep. VPI-AOE-161. VPI, Blacksburg VA.
Chow, J. S., Zilliac, G. G. & Bradshaw, P.
1994
Turbulence measurements in the near-field of a wingtip vortex.
ASME Forum on Turbulence in Complex Flows, Chicago IL, Nov. 6–11.
Ciffone, D. L.
1974
Correlation for estimating vortex rotational velocity downstream dependence.
J. Aircraft
11,
716–717.
Ciffone, D. L. & Orloff, K. L.
1975
Far-field wake-vortex characteristics of wings.
J. Aircraft
12,
464–470.
Corsiglia, V. R., Iversen, V. J. & Ciffone, D. L.
1976
Experimental study of the effect of span loading on aircraft wakes.
J. Aircraft
13,
968–973.
Corsiglia, V. R., Schwind, R. G. & Chigier, N. A.
1973
Rapid scanning, three-dimensional hotwire anemometer surveys of wing-tip vortices.
J. Aircraft
10,
752–757.
Devenport, W. J., Glegg, S. A. L. & Sharma, G.
1992
Turbulence measurements in trailing vortices for BWI noise prediction.
Rep. VPI-AOE-192. VPI, Blacksburg VA.
Devenport, W. J. & Sharma, G.
1990
Flow visualizations of a wing-tip vortex in the presence of a probe.
Rep. VPI-AOE-177. VPI, Blacksburg VA.
Döbbeling, K., Lenze, B. & Leuckel, W.
1990
Computer-aided calibration with a quadruple hotwire probe.
Exps. Fluids
8,
257–262.
Donaldson, C.duP.
1972
Calculation of turbulent shear flows for atmospheric and vortex motions.
AIAA J.
10,
4–12.
Donaldson, C.duP., Snedeker, R. S. & Sullivan, R. D.
1974
Calculation of aircraft wake velocity profiles and comparison with experimental measurements.
J. Aircraft
11,
547–555.
Dosanjh, D. S., Gasparek, E. P. & Eskinazi, S.
1962
Decay of a viscous vortex.
Aero. Q.
13,
167–188.
Engel, M.
1995
A wind-tunnel investigation of a wing-tip trailing vortex. 1 thesis,
AOE Dept, VPI, Blacksburg, VA.
Francis, T. B. & Katz, J.
1988
Observations on the development of a tip vortex on a rectangular hydrofoil.
Trans. ASME I: J. Fluids Engng
110,
208–215.
Garodz, L. J.
1971
Federal Aviation Administration full-scale aircraft vortex wake turbulence flight test investigations: past, present, and future.
AIAA Paper
71–97.
Gasparek, E. P.
1957
Viscous decay of a vortex. 1 thesis,
Syracuse University, NY.
Green, S.I. & Acosta, A. J.
1991
Unsteady flow in trailing vortices.
J. Fluid Mech.
227,
107–134.
Hoffman, E. R. & Joubert, P. N.
1963
Turbulent line vortices.
J. Fluid Mech.
16,
395–411.
Huffaker, R. M., Jelalian, A. V. & Thompson, J. A. L.
1970
Laser Doppler system for detection of aircraft trailing vortices.
Proc. IEEE
58,
322–326.
Iversen, J. D.
1976
Correlation of turbulent trailing vortex decay data.
J. Aircraft
13,
338–342.
Iversen, J. D., Corsiglia, V. R., Park, S., Backhus, D. R. & Brickman, R. A.
1979
Hot-wire, laser-anemometer, and force measurements of interacting trailing vortices.
J. Aircraft
16,
448–454.
Katz, J. & Bueno Galdo, J.
1989
Effect of roughness on rollup of tip vortices on a rectangular hydrofoil.
J. Aircraft
26,
247–253.
Kovasznay, L. S. G.
1954
Physical Measurements in Gas Dynamics and Combustion, p. 227.
Princeton University Press.
Leuptow, R. M., Breuer, K. S. & Haritonidis, J.H.
1988
Computer-aided calibration of X-probes using a look-up table.
Exps Fluids
7,
201–208.
Lezius, D. K.
1974
Water tank study of the decay of trailing vortices.
AIAA J.
12,
1065–1071.
Lundgren T. S. & Ashurst, W. T.
1989
Area-varying waves on curved vortex tubes with application to vortex breakdown.
J. Fluid Mech.
200,
283–307.
Marshall, J. S.
1993
The effect of axial pressure gradient on axisymmetrical and helical vortex waves.
Phys. Fluids A
5,
588–599.
Mason, W. H. & Marchman, J. F.
1972
Far-field structure of an aircraft trailing vortex.
NASA CR
62078.
Mason, W. H. & Marchman, J. F.
1973
Far-field structure of aircraft wake turbulence.
J. Aircraft
10,
86–92.
Mathioudakis, K. & Breugelmans, F. A. E.
1985
Use of triple hot wires to measure unsteady flows with large direction changes.
J. Phys. E: Sci. Instrum.
18,
414–419.
Maxworthy, T.
1988
Waves on vortex cores.
Fluid Dyn. Res.
3,
52–62.
Maxworthy, T., Hopfinger, E. J. & Redekopp, L. G.
1985
Wave motions on vortex cores.
J. Fluid Mech.
151,
141–165.
Mayer, E. W. & Powell, K. G.
1992
Similarity solutions for viscous vortex cores.
J. Fluid Mech.
238,
487–507.
McCormick, B. W., Tangler, J. L. & Sherrieb, H. E.
1968
Structure of trailing vortices.
J. Aircraft
5,
260–267.
Melander, M. V. & Hussain, F.
1991
Coherent structure dynamics: Interaction between large and fine scales.
8th Symp. on Turbulent Shear Flows, Munich, Sept. 9–11, Paper
28–5.
Mertaugh, L. J., Damania, R. B. & Paillet, F. L.
1977
An investigation of the near-field wake behind a full-scale test aircraft.
J. Aircraft
14,
894–902.
Monaghan, J. J. & Humble, R. J.
1993
Vortex particle methods for periodic channel flow.
J. Comput. Phys.
107,
152–159.
Orloff, K. L.
1974
Trailing vortex wind-tunnel diagnostics with a laser velocimeter.
J. Aircraft
11,
477–482.
Panton, R. L., Oberkampf, W. L. & Soskic, N.
1980
Flight measurements of a wing tip vortex.
J. Aircraft
17,
250–259.
Phillips, W. R. C. & Graham, J. A. H.
1984
Reynolds stress measurements in a turbulent trailing vortex.
J. Fluid Mech.
147,
353–371.
Ragab, S.
1995
Direct numerical simulation of instability waves in a trailing vortex.
AIAA Paper 95-0591.
Ragab, S. & Sreedhar, M.
1995
Numerical simulation of vortices with axial velocity deficits.
Phys. Fluids
7,
549–558.
Reed, R. E.
1973
Properties of the lateral random oscillations of trailing vortices observed in wind-tunnel tests.
Nielsen Engineering, NEAR TR-47, January.
Rossow, V. J.
1973
On the inviscid rolled-up structure of lift-generated vortices.
J. Aircraft
10,
647–650.
Sarpkaya, T.
1992
Three-dimensional interactions of vortices with a free surface.
AIAA Paper 92-0059.
Shekarriz, A., Fu, T. C., Katz, J. & Huang, T. T.
1993
Near-field behavior of a tip vortex.
AIAA J.
31,
112–118.
Singh, P. I. & Uberoi, M. S.
1976
Experiments on vortex stability.
Phys. Fluids
19
1858–1863
1858–1863.
Smits, A. J. & Kummer, R. P.
1985
The interaction and merger of two turbulent line vortices.
AIAA Paper 85-0046.
Steger, J. L. & Cutler, P.
1976
Implicit finite-difference procedures for the computation of vortex wakes.
AIAA Paper 76-385.
Stifle, K. E. & Panton, R. L.
1991
Experiments concerning the theories of vortex breakdown.
AIAA Paper 91-0736.
Stinebring, D. R., Farell, K. J. & Billet, M. L.
1991
The structure of a three-dimensional tip vortex at high Reynolds numbers.
Trans. ASME Fluids Engng
113,
496–503.
Thompson, D. H.
1975
Experimental study of axial flow in wing tip vortices.
J. Aircraft
8,
910–911.
Tutu, N. K. & Chevray, R.
1975
Cross-wire anemometry in high-intensity turbulence.
J. Fluid Mech.
71,
785–800.
Vogel, C. M., Devenport, W. J. & Zsoldos, J. S.
1995
Turbulence structure of a pair of merging tip vortices.
10th Symp. on Turbulent Shear Flows, Pennsylvania State University, August 14–16.
Vukoslavčević, P. & Wallace, J. M.
1981
Influence of velocity gradients on measurements of velocity and streamwise vorticity with hot-wire X-array probes.
Rev. Sci. Instrum.
52,
869–879.
Wood, N. B.
1975
A method for the determination and control of the frequency response of a constant-temperature hot-wire anemometer.
J. Fluid Mech.
67,
769–786.
Wygnanski, I., Champagne, F. & Marasli, B.
1986
On the large scale structures in two-dimensional small-deficit turbulent wakes.
J. Fluid Mech.
168,
31–71.
Zeman, O.
1995
The persistence of trailing vortices: a modelling study.
Phys. Fluids
7,
135–143.
Zheng, Y.
1992
An experimental study of wing-tip vortex in the near wake of a rectangular wing. PhD dissertation, Washington State University.
Zsoldos, J. S. & Devenport, W. J.
1991
Flow visualizations of interacting wing-tip vortex pairs.
Rep. VPI-AOE-188. VPI, Blacksburg VA.
Zsoldos, J. S. & Devenport, W. J.
1992
An experimental investigation of interacting trailing vortex pairs.
Proc. 19th Symp. on Naval Hydrodynamics,
Seoul, South Korea, August.
