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Experiments in Fluids

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01.08.2018 | Research Article

Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack

verfasst von: S. V. Lukashevich, S. O. Morozov, A. N. Shiplyuk

Erschienen in: Experiments in Fluids | Ausgabe 8/2018

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Abstract

Experimental investigations are performed to understand the effect of the passive porous coating on the high-frequency disturbances and laminar–turbulent transition of a hypersonic boundary layer on the sharp cone with an apex half-angle Θ_c = 7° aligned at normalized angles of attack up to α = 1° at the Mach number M_∞ = 5.8. It is demonstrated that the passive porous coating effectively suppresses the most unstable second-mode disturbances in the hypersonic boundary layer at the studied angles of attack. It is found that the passive porous coating delays the laminar–turbulent transition both on the windward and leeward sides. The reflection coefficient of the passive porous coating for ultrasonic acoustic waves is also measured.

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Vorheriger Artikel Multiple control modes of nanosecond-pulse-driven plasma-actuator evaluated by forces, static pressure, and PIV measurements

Nächster Artikel Jet mixing optimization using machine learning control

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Bres 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 MathSciNetCrossRefMATH

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 CrossRefMATH

Buttsworth DR, Jones TV (1997) Radial conduction effects in transient heat transfer experiments. Aeronaut J 101(1005):209–212. https://doi.org/10.1017/S0001924000066380

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 CrossRef

Cook WJ, Felderman EJ (1966) Reduction of data from thin-film heat-transfer gages: a concise numerical technique. AIAA J 4(3):561–562. https://doi.org/10.2514/3.3486 CrossRef

DiCristina V (1970) Three-dimensional laminar boundary-layer transition on a sharp 8° cone at Mach 10. AIAA J 8(5):852–856. https://doi.org/10.2514/3.5777 CrossRef

Fay J, Riddell F (1958) Theory of stagnation point heat transfer in dissociated air. J Aeronaut Sci 25(2):73–85. https://doi.org/10.2514/8.7517 MathSciNet

Fedorov AV, Yumashev DV (2005) Theoritical analysis of acoustic instability of a hypersonic shock layer on a porous wall. J Appl Mech Tech Phys 46(1):33–41. https://doi.org/10.1007/s10808-005-0005-9 MathSciNetCrossRefMATH

Fedorov AV, Malmuth ND, Rasheed A, Hornung HG (2001) Stabilization of hypersonic boundary layers by porous coatings. AIAA J 39(4):605–610. https://doi.org/10.2514/2.1382 CrossRef

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 CrossRefMATH

Fedorov AV, Kozlov VF, Addison RC (2008) Reflection of acoustic disturbances from a porous coating of regular microstructure. In: 5th AIAA Theoretical Fluid Mechanics Conference, AIAA Paper 2008-3902

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 CrossRef

Laurence SJ, Wagner A, Hannemann K (2016) Experimental study of second-mode instability growth and breakdown in a hypersonic boundary layer using high-speed schlieren visualization. J Fluid Mech 797:471–503. https://doi.org/10.1017/jfm.2016.280 CrossRef

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 CrossRef

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 CrossRef

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 CrossRef

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 CrossRef

Marineau EC, Moraru CG, Lewis DR, Norris JD, Lafferty JF, Wagnild RM, Smith JA (2014) Mach 10 boundary-layer transition experiments on sharp and blunted cones. AIAA Paper 2014-3108

Marineau EC, Moraru CG, Lewis DR, Norris JD, Lafferty JF, Johnson HB (2015) Investigation of Mach 10 boundary layer stability of sharp cones at angle-of-attack, part 1: Experiments. In: 53rd AIAA Aerospace Sciences Meeting, AIAA Paper 2015-1737. https://doi.org/10.2514/6.2015-1737

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 CrossRef

Stetson KF (1982) Mach 6 experiments of transition on a cone at angle of attack. J Spacecr Rockets 19(5):397–403. https://doi.org/10.2514/3.62276 CrossRef

Stetson KF, Thompson ER, Donaldson JC, Siler LG (1985) Laminar boundary layer stability experiments on a cone at Mach 8. Part III: sharp cone at angle of attack. In: 23rd Aerospace Sciences Meeting AIAA-85-0492

Tritarelli RC, Lele SK, Fedorov A (2015) Stabilization of a hypersonic boundary layer using a felt-metal porous coating. J Fluid Mech 769:729–739. https://doi.org/10.1017/jfm.2015.156 CrossRef

Tsyryulnikov IS, Maslov AA, Mironov SG, Poplavskaya TV, Kirilovskiy SV (2015) The efficiency of the method of sound-absorbing coatings in vibrationally excited hypersonic flow. Tech Phys Lett 41(2):184–186. https://doi.org/10.1134/S1063785015020273 CrossRef

Vipin M, Stephen SO (2012) Nonlinear stability of hypersonic flow over a cone with passive porous walls. J Fluid Mech 713:528–563. https://doi.org/10.1017/jfm.2012.472 MathSciNetCrossRefMATH

Wadhams TP, MacLean MG, Holden MS, Mundy E (2007) Pre-flight ground testing of the full-scale FRESH FX-1 at fully duplicated flight conditions. In: 37th AIAA Fluid Dynamics Conference. AIAA Paper 2007-4488

Wagner A, Hannemann K, Wartemann V, Giese T (2013) Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material Part 1: Experimental results. In: 51st AIAA Aerospace Sciences Meeting. AIAA Paper 2013-270

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 CrossRef

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 MathSciNetCrossRef

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 CrossRef

Wartemann V, Wagner A, Giese T, Eggers T, Hannemann K (2014) Boundary-layer stabilization by an ultrasonically absorptive material on a cone in hypersonic flow: Numerical investigations. CEAS Space J 6(1):13–22. https://doi.org/10.1007/s12567-013-0053-6 CrossRef

Titel: Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack
verfasst von: S. V. Lukashevich
S. O. Morozov
A. N. Shiplyuk
Publikationsdatum: 01.08.2018
Verlag: Springer Berlin Heidelberg
Erschienen in: Experiments in Fluids / Ausgabe 8/2018
Print ISSN: 0723-4864
Elektronische ISSN: 1432-1114
DOI: https://doi.org/10.1007/s00348-018-2585-1

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