Hypersonic Boundary Layer Instability and Control by Passive Porous Coatings
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-67902-6_53
Reference9 articles.
1. Buntin, D.A., Lukashevich, S.V., Maslov, A.A., Shiplyuk, A.N.: Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer. Fluid Dyn. 45(6), 898–904 (2010). https://doi.org/10.1134/S0015462810060074
2. Cook, W.J., Felderman, E.J.: Reduction of data from thin-film heat-transfer gages: a concise numerical technique. AIAA J 4(3), 561–562 (1966). https://doi.org/10.2514/3.3486
3. Fedorov, A.V., Malmuth, N.D., Rasheed, A., Hornung, H.G.: Stabilization of hypersonic boundary layers by porous coatings. AIAA J. 39(4), 605–610 (2001). https://doi.org/10.2514/2.1382
4. Fedorov, A.V., Shiplyuk, A.N., Maslov, A.A., Burov, E.V., Malmuth, N.D.: Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating. J. Fluid Mech. 479, 99–124 (2003). https://doi.org/10.1017/S0022112002003440
5. Lukashevich, S.V., Morozov, S.O., Shiplyuk, A.N.: 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
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