12 results
Wall-pressure fluctuations in an axisymmetric boundary layer under strong adverse pressure gradient
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- Journal of Fluid Mechanics / Volume 960 / 10 April 2023
- Published online by Cambridge University Press:
- 05 April 2023, A28
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The structure of a highly decelerated axisymmetric turbulent boundary layer
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- Journal of Fluid Mechanics / Volume 929 / 25 December 2021
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- 19 October 2021, A9
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Characteristics of the pressure fluctuations generated in turbulent boundary layers over rough surfaces
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- Journal of Fluid Mechanics / Volume 883 / 25 January 2020
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- 20 November 2019, A3
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Aeroacoustics of a rotor ingesting a planar boundary layer at high thrust
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- Journal of Fluid Mechanics / Volume 850 / 10 September 2018
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- 04 July 2018, pp. 212-245
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The wall-pressure spectrum of high-Reynolds-number turbulent boundary-layer flows over rough surfaces
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- Journal of Fluid Mechanics / Volume 768 / 10 April 2015
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- 09 March 2015, pp. 261-293
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Pressure fluctuations produced by forward steps immersed in a turbulent boundary layer
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- Journal of Fluid Mechanics / Volume 756 / 10 October 2014
- Published online by Cambridge University Press:
- 02 September 2014, pp. 384-421
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CORRIGENDA
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- Journal of Fluid Mechanics / Volume 326 / 10 November 1996
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- 26 April 2006, p. 437
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The structure and development of a wing-tip vortex
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- Journal of Fluid Mechanics / Volume 312 / 10 April 1996
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- 26 April 2006, pp. 67-106
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The diode-array velocimeter
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- Journal of Fluid Mechanics / Volume 259 / 25 January 1994
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- 26 April 2006, pp. 167-189
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Time-depeiident and time-averaged turbulence structure near the nose of a wing-body junction
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- Journal of Fluid Mechanics / Volume 210 / January 1990
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- 26 April 2006, pp. 23-55
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Flow structure produced by the interaction and merger of a pair of co-rotating wing-tip vortices
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- Journal of Fluid Mechanics / Volume 394 / 10 September 1999
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- 10 September 1999, pp. 357-377
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The structure and development of a counter-rotating wing-tip vortex pair
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- Journal of Fluid Mechanics / Volume 332 / February 1997
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- 10 February 1997, pp. 71-104
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