Abstract
Effect of leading-edge anisotropic erosion (negative skewness) and deposition (positive skewness) on a transitional separation bubble (TSB) is investigated using single-wire hot wire anemometer for a Reynolds number (Rec) of \(2.5 \times 10^{5}\), , based on the model chord and tunnel free stream velocity. Three different models are fabricated for investigation, whose surfaces are smooth (SS), sand blasted (BS) and sand deposited (DS), respectively. The fabricated rough surfaces are three-dimensionally irregular and replicate the anisotropic pattern of an operationally deteriorated turbine blade due to chronic exposure to harsh working environments. Results of positive and negative skewed rough surfaces are compared with that of smooth surface. The bubble is observed to be shortened by about 35% and 10% of that formed over SS for DS and BS, respectively. Premature transition is observed on DS, which is 49% earlier than BS case. Though the transition point varies, it is interesting to note that the chord length occupied by the transition and turbulent region of the bubble is almost same for all the cases. Presumably, more than the negatively skewed anisotropic rough surface, the positive counterpart tends to influence the boundary layer stability and thereby the transition characteristic of separation bubble.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Abbreviations
- c:
-
Chord length of flat plate model [mm]
- D:
-
Leading-edge diameter of the flat plate model [mm]
- \(H_{12}\):
-
Boundary layer shape factor
- \({\text{Re}}_{c}\):
-
Reynolds number based on the chord of the flat plate model
- \({\text{Re}}_{{\delta_{2,S} }}\):
-
Reynolds number based on momentum thickness at separation
- \({\text{Re}}_{{l_{1} }}\):
-
Transitional Reynolds number (based on transitional length of TSB)
- \(l_{b}\):
-
Mean length of TSB [mm]
- \(l_{0}\):
-
Length of laminar portion of TSB [mm]
- \(l_{1}\):
-
Length of transitional portion of TSB [mm]
- \(l_{2}\):
-
Length of turbulent portion of TSB [mm]
- \(\overline{u}\):
-
Streamwise mean velocity [m/s]
- \(U_{e}\):
-
Boundary layer edge velocity [m/s]
- \(u_{{{\text{rms}}}}\):
-
Root-mean-squared fluctuation of streamwise velocity [m/s]
- \(u_{{{\text{rms}}_{{{\text{max}}}} }}\):
-
Maximum of local rms fluctuation of streamwise velocity [m/s]
- \(x_{T^{\prime}}\):
-
Streamwise location of onset of transition [mm]
- \(x_{T}\):
-
Streamwise location of end of transition (or) point of transition [mm]
- \(x_{R}\):
-
Streamwise location of reattachment [mm]
- \(\gamma\):
-
Separation angle [o]
- \(\delta_{1}\):
-
Displacement thickness of boundary layer [mm]
- \(\delta_{2}\):
-
Momentum thickness of boundary layer [mm]
- \(\delta_{{1_{t} }} /\delta_{{2_{s} }}\):
-
Proximity parameter (Displacement thickness at transition/Momentum thickness at separation)
References
Fitzgerald EJ, Mueller TJ (1990) Measurements in a separation bubble on an airfoil using laser velocimetry. AIAA J 28(4):584–592
Hatman A, Wang T (1998) Separated-flow transition part 1—experimental methodology and mode classification, paper no. 98-GT-461, international gas turbine and aeroengine congress and exhibition. Stockholm, Sweden
Sandham ND (2008) Transitional separation bubbles and unsteady aspects of aerofoil stall. Aeronaut J 112(1133):395–404
Serna J, Lázaro BJ (2015) On the laminar region and the initial stages of transition in transitional separation bubbles. Eur J Mech, B/Fluids. 49(Part A):171–183
Mueller TJ, DeLaurier JD (2003) Aerodynamics of small vehicles. Annu Rev Fluid Mech 35:89–111
Han W, Kim J, Kim B (2018) Effects of contamination and erosion at the leading edge of blade tip airfoils on the annual energy production of wind turbines. Renew Energy 115:817–823
Bons JP, Taylor RP, McClain ST, Rivir RB (2001) The many faces of turbine surface roughness. J Turbomach 123(4):739–748
Ravishankara AK, Özdemir H, van der Weide E (2021) Analysis of leading edge erosion effects on turbulent flow over airfoils. Renew Energy 172:765–779
Bons JP (2010) A review of surface roughness effects in gas turbines. J Turbomach 132(2):1–16
Laguna-Camacho JR, Villagrán-Villegas LY, MartÃnez-GarcÃa H, Juárez-Morales G, Cruz-Orduña MI, Vite-Torres M, RÃos-Velasco L, Hernández-Romero I (2016) A study of the wear damage on gas turbine blades. Eng Fail Anal 61:88–99
Hamed A, Tabakoff W, Wenglarz R (2006) Erosion and deposition in turbomachinery. J Propul Power 22(2):350–360
Gaster M (1967) The structure and behaviour of laminar separation bubbles, reports & memoranda no. 3595. Aeronautical research council, pp 1–31
Horton HP (1969) A semi-empirical theory for the growth and bursting of laminar separation bubbles, current paper no. 1073. Aeronautical research council, pp 1–44
Arena AV, Mueller TJ (1980) Laminar separation, transition, and turbulent reattachment near the leading edge of airfoils. AIAA J 18(7):747–753
Brendel M, Mueller TJ (1987) Boundary-layer measurements on an airfoil at low Reynolds numbers. J Aircr 25(7):612–617
O’Meara MM, Mueller TJ (1987) Laminar separation bubble characteristics on an airfoil at low Reynolds numbers. AIAA J 25(8):1033–1041
Serna J, Lázaro BJ (2014) The final stages of transition and the reattachment region in transitional separation bubbles. Exp Fluids 55(9):1–17
Anand K, Sarkar S (2017) Features of a laminar separated boundary layer near the leading-edge of a model airfoil for different angles of attack: an experimental study. J Fluids Eng, Trans ASME 139(2):1–14
Tuna BA, Kurelek JW, Yarusevych S (2019) Surface-pressure-based estimation of the velocity field in a separation bubble. AIAA J 57(9):3825–3837
Legner HH (1983) A review of roughness-induced nosetip transition. AIAA J 21(1):7–22
Kerho MF, Bragg MB (1997) Airfoil boundary-layer development and transition with large leading-edge roughness. AIAA J 35(1):75–84
Downs RS, White EB, Denissen NA (2008) Transient growth and transition induced by random distributed roughness. AIAA J 46(2):451–462
Simens MP, Gungor AG (2014) The effect of surface roughness on laminar separated boundary layers. J Turbomach 136(3):1–8
Sengupta A, Vadlamani NR, Tucker P (9–13 Jan 2017) Roughness induced transition in low pressure turbines, paper no. AIAA 2017-0303, AIAA SciTech forum—55th AIAA aerospace sciences meeting. Grapevine, Texas
Bons JP, Christensen KT (25–28 June 2007) A comparison of real and simulated surface roughness characterizations, paper no. AIAA 2007-3997, 37th AIAA fluid dynamics conference. Miami, Florida
Napoli E, Armenio V, De Marchis M (2008) The effect of the slope of irregularly distributed roughness elements on turbulent wall-bounded flows. J Fluid Mech 613:385–394
Bhaganagar K, Chau L (2015) Characterizing turbulent flow over 3-D idealized and irregular rough surfaces at low Reynolds number. Appl Math Model 39(22):6751–6766
Bulaha N, Rudzitis J (2018) Calculation possibilities of 3D parameters for surfaces with irregular roughness. Latv J Phys Tech Sci 55(4):70–79
Busse A, Thakkar M, Sandham ND (2017) Reynolds-number dependence of the near-wall flow over irregular rough surfaces. J Fluid Mech 810:196–224
Busse A, Jelly TO (2020) Influence of surface anisotropy on turbulent flow over irregular roughness. Flow Turbul Combust 104:331–354
Amarloo A, Forooghi P, Abkar M (2022) Secondary flows in statistically unstable turbulent boundary layers with spanwise heterogeneous roughness. Theor Appl Mech Lett 12(2):1–7
de Marchis M, Napoli E, Armenio V (2010) Turbulence structures over irregular rough surfaces 11(3):1–32
Volino RJ, Hultgren LS (2001) Measurements in separated and transitional boundary layers under low-pressure turbine airfoil conditions. J Turbomach 123(2):189–197
Serna J, Lázaro BJ (2015) On the bursting condition for transitional separation bubbles. Aerosp Sci Technol 44:43–50
Diwan SS, Ramesh ON (2007) Laminar separation bubbles: dynamics and control. Sadhana—Acad Proc Eng Sci 32:103–109
Acknowledgements
The present work is part of the research project funded by DST-SERB, New Delhi (File No.: EMR/2016/005834). Also, the resources offered by SASTRA management is sincerely acknowledged.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2024 The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Ganesh, K.T., Anand, K. (2024). Characteristics of Transitional Separation Bubble Formed Over Negatively and Positively Skewed Anisotropic Rough Surface. In: Singh, K.M., Dutta, S., Subudhi, S., Singh, N.K. (eds) Fluid Mechanics and Fluid Power, Volume 2. FMFP 2022. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-99-5752-1_8
Download citation
DOI: https://doi.org/10.1007/978-981-99-5752-1_8
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-99-5751-4
Online ISBN: 978-981-99-5752-1
eBook Packages: EngineeringEngineering (R0)