Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up

R. Schook; C.J. Hogendoorn; H.C. Lange, de; A.A. Steenhoven, van

Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up

R. Schook
, C.J. Hogendoorn
, H.C. Lange, de
, A.A. Steenhoven, van

Energy Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

Abstract

The effect of compressibility on boundary layer transition is studied by using a Ludwieg tube set-up. Heat transfer expts. are performed at a flat plate using thin film gauges. The expts. are done with Mach nos. ranging from 0.13 to 0.56. The dimensions of the turbulence grid are not changed. This results in a decrease of the turbulence level with increasing Mach no. No significant change of transition start or transition length as a function of the Mach no. is obsd. However, as measured sep. the turbulence level has a significant influence on both mentioned transition parameters. From this turbulence level and Mach no. have an opposite effect on boundary layer transition

Original language	English
Title of host publication	Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997
Editors	K. Hanjalic, T.W.J. Peeters
Place of Publication	Delft
Publisher	Delft University Press
Pages	229-236
ISBN (Print)	90-407-1465-7
Publication status	Published - 1997

Cite this

Schook, R., Hogendoorn, C. J., Lange, de, H. C., & Steenhoven, van, A. A. (1997). Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up. In K. Hanjalic, & T. W. J. Peeters (Eds.), Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997 (pp. 229-236). Delft University Press.

Schook, R. ; Hogendoorn, C.J. ; Lange, de, H.C. et al. / Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up. Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997. editor / K. Hanjalic ; T.W.J. Peeters. Delft : Delft University Press, 1997. pp. 229-236

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title = "Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up",

abstract = "The effect of compressibility on boundary layer transition is studied by using a Ludwieg tube set-up. Heat transfer expts. are performed at a flat plate using thin film gauges. The expts. are done with Mach nos. ranging from 0.13 to 0.56. The dimensions of the turbulence grid are not changed. This results in a decrease of the turbulence level with increasing Mach no. No significant change of transition start or transition length as a function of the Mach no. is obsd. However, as measured sep. the turbulence level has a significant influence on both mentioned transition parameters. From this turbulence level and Mach no. have an opposite effect on boundary layer transition",

author = "R. Schook and C.J. Hogendoorn and \{Lange, de\}, H.C. and \{Steenhoven, van\}, A.A.",

year = "1997",

language = "English",

isbn = "90-407-1465-7",

pages = "229--236",

editor = "K. Hanjalic and T.W.J. Peeters",

booktitle = "Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997",

publisher = "Delft University Press",

}

Schook, R, Hogendoorn, CJ, Lange, de, HC & Steenhoven, van, AA 1997, Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up. in K Hanjalic & TWJ Peeters (eds), Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997. Delft University Press, Delft, pp. 229-236.

Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up. / Schook, R.; Hogendoorn, C.J.; Lange, de, H.C. et al.
Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997. ed. / K. Hanjalic; T.W.J. Peeters. Delft: Delft University Press, 1997. p. 229-236.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

TY - GEN

T1 - Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up

AU - Schook, R.

AU - Hogendoorn, C.J.

AU - Lange, de, H.C.

AU - Steenhoven, van, A.A.

PY - 1997

Y1 - 1997

N2 - The effect of compressibility on boundary layer transition is studied by using a Ludwieg tube set-up. Heat transfer expts. are performed at a flat plate using thin film gauges. The expts. are done with Mach nos. ranging from 0.13 to 0.56. The dimensions of the turbulence grid are not changed. This results in a decrease of the turbulence level with increasing Mach no. No significant change of transition start or transition length as a function of the Mach no. is obsd. However, as measured sep. the turbulence level has a significant influence on both mentioned transition parameters. From this turbulence level and Mach no. have an opposite effect on boundary layer transition

AB - The effect of compressibility on boundary layer transition is studied by using a Ludwieg tube set-up. Heat transfer expts. are performed at a flat plate using thin film gauges. The expts. are done with Mach nos. ranging from 0.13 to 0.56. The dimensions of the turbulence grid are not changed. This results in a decrease of the turbulence level with increasing Mach no. No significant change of transition start or transition length as a function of the Mach no. is obsd. However, as measured sep. the turbulence level has a significant influence on both mentioned transition parameters. From this turbulence level and Mach no. have an opposite effect on boundary layer transition

M3 - Conference contribution

SN - 90-407-1465-7

SP - 229

EP - 236

BT - Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997

A2 - Hanjalic, K.

A2 - Peeters, T.W.J.

PB - Delft University Press

CY - Delft

ER -

Schook R, Hogendoorn CJ, Lange, de HC , Steenhoven, van AA. Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up. In Hanjalic K, Peeters TWJ, editors, Turbulence, heat and mass transfer 2 : proceedings of the international symposium on turbulence, heat and mass transfer, Delft, The Netherlands, June 9-12, 1997. Delft: Delft University Press. 1997. p. 229-236

Influence of the Mach number on boundary layer transition by a Ludwieg tube set-up

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