Abstract
The effect of surfaces with streamwise microgrooves on the development of natural disturbances in a hypersonic boundary layer is experimentally studied. The experiments are performed on a sharp cone at the free-stream Mach number M∞ = 5.8. Microgrooves with rectangular and triangular cross sections are considered. The pressure fluctuations are measured on the cone surface at two stations upstream and downstream of the section with grooved surfaces. It is shown that the peak amplitude of the second-mode disturbances is much lower on the surface with microgrooves than on the solid surface, and the first-mode amplitude is always higher than that on the solid surface. It is found that the efficiency of stabilization of the second-mode disturbances depends on the groove depth and porosity. The greatest effect of stabilization is reached with the groove depth of about one quarter of the second-mode wave length. The growth rate of the first-mode disturbances is greater on the surfaces with microgrooves than on the solid surface.
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Anderson BP, Campbell CH, Saucedo LA, Kinder GR, Berger KT (2010) Boundary layer transition flight experiment overview and in-situ measurements. AIAA Paper 2010-240
Bountin DA, Sidorenko AA, Shiplyuk AN (2001) Development of natural disturbances in a hypersonic boundary layer on a sharp cone. J Appl Mech Technol Phys 42(1):57–62. https://doi.org/10.1023/A:1018852410488
Bountin D, Chimitov T, Maslov A, Novikov A, Egorov I, Fedorov A, Utyuzhnikov S (2013) Stabilization of a hypersonic boundary layer using a wavy surface. AIAA J 51(5):1203–1210. https://doi.org/10.2514/1.J052044
Bres GA, Colonius T, Fedorov AV (2010) Acoustic properties of porous coatings for hypersonic boundary-layer control. AIAA J 48(2):267–274. https://doi.org/10.2514/1.40811
Brès GA, Inkman M, Colonius T, Fedorov AV (2013) Second-mode attenuation and cancellation by porous coatings in a high-speed boundary layer. J Fluid Mech 726:312–337. https://doi.org/10.1017/jfm.2013.206
Buntin DA, Lukashevich SV, Maslov AA, Shiplyuk AN (2010) Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer. Fluid Dyn 45(6):898–904. https://doi.org/10.1134/S0015462810060074
Camillo GP, Wagner A, Dittert C et al (2020) Experimental investigation of the effect of transpiration cooling on second mode instabilities in a hypersonic boundary layer. Exp Fluids 61:162. https://doi.org/10.1007/s00348-020-02994-8
Chokani N, Bountin DA, Shiplyuk AN, Maslov AA (2005) Nonlinear aspects of hypersonic boundary-layer stability on a porous surface. AIAA J 43(1):149–155. https://doi.org/10.2514/1.9547
Demetriades A (1974) Hypersonic viscous flow over a slander cone. Part III: Laminar instability and transition. AIAA Paper 1974-535
Fedorov AV (2011) Transition and stability of high-speed boundary layers. Annu Rev Fluid Mech 43:79–95. https://doi.org/10.1146/annurev-fluid-122109-160750
Fedorov A, Shiplyuk A, Maslov A, Burov E, Malmuth N (2003) Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating. J Fluid Mech 479:99–124. https://doi.org/10.1017/S0022112002003440
Fedorov A, Soudakov V, Egorov I, Sidorenko A, Gromyko Y, Bountin D, Polivanov P, Maslov A (2015) High-speed boundary-layer stability on a cone with localized wall heating or cooling. AIAA J 53(9):2512–2524. https://doi.org/10.2514/1.J053666
Fedorov AV, Novikov AV, Semenov NN (2020) Toward optimal wavy surface shape for high-speed boundary layer stabilization. Int J Fluid Mech Res 47(4):329–335. https://doi.org/10.1615/InterJFluidMechRes.2020033001
Fong KD, Wang X, Huang Y, Zhong X, McKiernan GR, Fisher RA, Schneider SP (2015) Second mode suppression in hypersonic boundary layer by roughness: design and experiments. AIAA J 53(10):3138–3144. https://doi.org/10.2514/1.J054100
Golubev IF (1970) Viscosity of gases and gas mixtures. Israel Program for Scientific Translations, Jerusalem
Gromyko YV, Polivanov PA, Sidorenko AA, Buntin DA, Maslov AA (2013) An experimental study of the natural noise in the transit-m hypersonic wind tunnel. Thermophys Aeromech 20(4):481–493. https://doi.org/10.1134/S0869864313040112
Gülhan A, Neeb D, Thiele T, Siebe F (2015) Aerothermal postflight analysis of the sharp edge flight experiment-II. J Spacecr Rockets 53(1):1–25. https://doi.org/10.2514/1.A33275
Haley C, Casper KM, Zhong X (2019) Joint numerical and experimental investigation of roughness effect on hypersonic 2nd mode instability and transition. AIAA Paper 2019–0873
Hao J, Wen CY (2019) Stabilization of a mach 6 boundary layer using a two-dimensional cavity. AIAA Paper 2019–1131
Kendall JM (1975) Wind tunnel experiments relating to supersonic and hypersonic boundary layer transition. AIAA J 13(3):290–299. https://doi.org/10.2514/3.49694
Lukashevich SV, Maslov AA, Shiplyuk AN, Fedorov AV, Soudakov VG (2012a) Stabilization of high-speed boundary layer using porous coatings of various thicknesses. AIAA J 50(9):1897–1904. https://doi.org/10.2514/1.J051377
Lukashevich SV, Morozov SO, Shiplyuk AN (2012b) Experimental study of the influence of parameters of a passive porous coating on the development of disturbances in a hypersonic boundary layer. Tech Phys Lett 38(12):1077–1079. https://doi.org/10.1134/S1063785012120073
Lukashevich SV, Morozov SO, Shiplyuk AN (2013) Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer. 1. Effect of the porous coating length. J App Mech Tech Phys 54(4):572–577. https://doi.org/10.1134/S002189441304007X
Lukashevich SV, Morozov SO, Shiplyuk AN (2016) Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer 2. Effect of the porous coating location. J App Mech Tech Phys 57(5):873–878. https://doi.org/10.1134/S002189441605014X
Lukashevich SV, Morozov SO, Shiplyuk AN (2017) Investigation of the influence of a slots depth on disturbances in a hypersonic boundary layer. AIP Conf Proc 1893:030032. https://doi.org/10.1063/1.5007490
Lukashevich SV, Morozov SO, Shiplyuk AN (2018a) Investigations of the influence of slots spacing and depth on second mode disturbances in hypersonic boundary layer. AIP Conf Proc 2027:040066. https://doi.org/10.1063/1.5065340
Lukashevich SV, Morozov SO, Shiplyuk AN (2018b) Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack. Exp Fluids 59(8):130. https://doi.org/10.1007/s00348-018-2585-1
Lukashevich SV, Morozov SO, Shiplyuk AN (2019) Stabilization of the high frequency disturbances in hypersonic boundary layer by the surfaces consisting of micro slots. AIP Conf Proc 2125:030021
Lysenko VI, Gaponov SA, Smorodsky BV, Yermolaev YG, Kosinov AD, Semionov NV (2016) Combined influence of coating permeability and roughness on supersonic boundary layer stability and transition. J Fluid Mech 798:751–773. https://doi.org/10.1017/jfm.2016.347
Mack LM (1975) Linear stability theory and the problem of supersonic boundary layer transition. AIAA J 13(3):278–289. https://doi.org/10.2514/3.49693
Malmuth ND, Fedorov AV, Shalaev VI, Cole J, Khokhlov AP, Hites M, Williams D (1998) Problems in high speed flow prediction relevant to control. AIAA Paper 1998–2695
Maslov A, Shiplyuk A, Sidorenko A, Polivanov P, Fedorov A, Kozlov V, Malmuth N (2006) Hypersonic laminar flow control using a porous coating of Random microstructure. AIAA Paper 2006–1112
Miró Miró F, Pinna F (2020) Injection-gas-composition effects on hypersonic boundary-layer transition. J Fluid Mech 890:1–14. https://doi.org/10.1017/jfm.2020.129
Morkovin MV (1969) On the many faces of transition. In: Wells CS (ed) Viscous drag reduction. Springer, Boston. https://doi.org/10.1007/978-1-4899-5579-1_1
Morozov SO, Lukashevich SV, Soudakov VG, Shiplyuk AN (2018) Experimental study of the influence of small angles of attack and cone nose bluntness on the stabilization of hypersonic boundary layer with passive porous coating. Thermophys Aeromech 25(6):793–800. https://doi.org/10.1134/S086986431806001X
Paredes P, Choudhari MM, Li F (2018) Transition delay via vortex generators in a hypersonic boundary layer at flight conditions. AIAA Paper 2018–3217
Paredes P, Choudhari MM, Li F (2019) Instability wave-streak interactions in a high Mach number boundary layer at flight conditions. J Fluid Mech 858:474–499. https://doi.org/10.1017/jfm.2018.744
Rasheed A, Hornung HG, Fedorov AV, Malmuth ND (2002) Experiments on passive hypervelocity boundary-layer control using an ultrasonically absorptive surface. AIAA J 40(3):481–489. https://doi.org/10.2514/2.1671
Reshotko E (1976) Boundary-layer stability and transition. Annu Rev Fluid Mech 8(1):311–349. https://doi.org/10.1146/annurev.fl.08.010176.001523
Sawaya J, Sassanis V, Yassir S, Sescu A, Visbal M (2018) Assessment of the impact of two-dimensional wall deformation shape on high-speed boundary-layer disturbances. AIAA J 56(12):4787–4800. https://doi.org/10.2514/1.J057045
Si W (2020) The influence of wavy wall on hypersonic boundary layer instability over a flared cone. Int J Mod Phys B 34(14–16):1–5. https://doi.org/10.1142/S0217979220400937
Sousa VCB, Patel D, Chapelier J, Wartemann V, Wagner A, Scalo C (2019) Numerical investigation of second-mode attenuation over carbon/carbon porous surfaces. J Spacecr Rockets 56(2):319–332. https://doi.org/10.2514/1.A34294
Stetson KF, Kimmel RL (1992) On hypersonic boundary-layer stability. AIAA Paper 1992–0737
Tian X, Zhao R, Long T, Wen CY (2019) Reverse design of ultrasonic absorptive coating for the stabilization of Mack modes. AIAA J 57(6):2264–2269. https://doi.org/10.2514/1.J058105
Wagner A, Hannemann K, Wartemann V, Giese T (2013a) Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material Part 1: experimental results. AIAA Paper 2013–270
Wagner A, Kuhn M, Martinez Schramm J et al (2013b) Experiments on passive hypersonic boundary layer control using ultrasonically absorptive carbon–carbon material with random microstructure. Exp Fluids 54:1606. https://doi.org/10.1007/s00348-013-1606-3
Wagner A, Hannemann K, Kuhn M (2014) Ultrasonic absorption characteristics of porous carbon-carbon ceramics with random microstructure for passive hypersonic boundary layer transition control. Exp Fluids 55(6):1750. https://doi.org/10.1007/s00348-014-1750-4
Wang X, Zhong X (2012) The stabilization of a hypersonic boundary layer using local sections of porous coating. Phys Fluids 24(3):034105. https://doi.org/10.1063/1.3694808
Wartemann V, Lüdeke H, Sandham ND (2012) Numerical investigation of hypersonic boundary-layer stabilization by porous surfaces. AIAA J 50(6):1281–1290. https://doi.org/10.2514/1.J051355
Zhao R, Liu T, Wen CY, Zhu J, Cheng L (2019) Impedance-near-zero acoustic metasurface for hypersonic boundary-layer flow stabilization. Phys Rev App. https://doi.org/10.1103/PhysRevApplied.11.044015
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The research was carried out within the framework of the Russian Science Foundation (Grant No. 21-19-00393).
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Lukashevich, S.V., Morozov, S.O. & Shiplyuk, A.N. Experiments on the development of natural disturbances in a hypersonic boundary layer on surfaces with microgrooves. Exp Fluids 62, 155 (2021). https://doi.org/10.1007/s00348-021-03250-3
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DOI: https://doi.org/10.1007/s00348-021-03250-3