2012
DOI: 10.1134/s1063785012120073
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Experimental study of the influence of parameters of a passive porous coating on the development of disturbances in a hypersonic boundary layer

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Cited by 9 publications
(7 citation statements)
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“…A further increase in the coating thickness did not lead to an increase in coating efficiency; the maximum degree of stabilization of the second mode for coatings with porosity values of 44 and 64% was almost identical. The results of calculations [11] performed for the test conditions of [10] agree well with the experimental data. Wartemann et al [12] reported the results of a numerical study of the effect of the pore shape and size on the character of flow disturbances, which also agree with our experimental data [10].…”
Section: Introductionsupporting
confidence: 73%
See 1 more Smart Citation
“…A further increase in the coating thickness did not lead to an increase in coating efficiency; the maximum degree of stabilization of the second mode for coatings with porosity values of 44 and 64% was almost identical. The results of calculations [11] performed for the test conditions of [10] agree well with the experimental data. Wartemann et al [12] reported the results of a numerical study of the effect of the pore shape and size on the character of flow disturbances, which also agree with our experimental data [10].…”
Section: Introductionsupporting
confidence: 73%
“…The effect of the thickness and degree of porosity of the passive porous coating on the second mode of disturbances was studied in [10]. The coating efficiency was demonstrated to increase as the porous coating thickness was increased up to a certain value.…”
Section: Introductionmentioning
confidence: 99%
“…Theoretical and experimental works show that using ultrasonic absorptive coating allows to reduce the intensity of most unstable ultrasonic disturbances (second mode disturbances) in hypersonic boundary layers [3][4][5][6][7][8][9]. Experimental investigations confirm that the ultrasonic absorptive coatings effectiveness depends on its depth [6,7].…”
Section: Introductionmentioning
confidence: 74%
“…The previous experimental studies are shown that it's possible either to reduce or magnify the energy of second mode disturbances using the porous coating with different length on the cone [11]. It indicates that the ability of the porous coating to delay transition is not predictable in case of small varying hypersonic boundary layer parameters.…”
Section: Introductionmentioning
confidence: 99%
“…The layers are turned with respect to each other by the angle of 45˚. The coating thickness are chosen as most effective according to the experimental work [11]. The thickness equals to 0.18 mm.…”
Section: Introductionmentioning
confidence: 99%