Leading-edge receptivity of a hypersonic boundary layer on a flat plate

By A. Maslov, A. Shiplyuk, A. Sidorenko, D. Arnal. Journal of Fluid Mechanics, 2001

164 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Ocean Engineering

View Paper: https://www.semanticscholar.org/paper/61c2be05c3bcaa39af8b9d41fc83057c65b866c8

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Citations in the corpus

Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers (2013, background): “Detailed recent experimental, theoretical and computational studies of high-speed receptivity can be found in the work of Maslov et al. (2001), Fedorov (2003) and Ma & Zhong (2003a,b, 2005).”
Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating (2003, methodology): “Maslov et al. (2001) have successfully applied this technique to hypersonic flows.”
Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances (2005, result): “Based on the first feature, they predicted that modes 1 and 2 can be effectively excited by acoustic waves near the leading-edge region, in qualitative agreement with the leading-edge receptivity experiment of a Mach 6 flow over a flat plate by Maslov et al. (2001).”
Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound (2003, background): “There have been a number of experimental studies on the receptivity of supersonic and hypersonic boundary layers (Maslov & Semionov 1986; Semionov, Kosinpv & Maslov 1996, 1998; Arnal et al. 1999; Maslov et al. 2001).”
Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions (2003, background): “Semionov et al. 1996, Arnal et al. 1999 and Maslov et al. (2001) also conducted experimental investigations of hypersonic boundary-layer receptivity, on the sharp leading edge of a flat plate, to acoustic waves in a Mach 5.92 flow in the free stream.”
Direct numerical simulation of transition in a sharp cone boundary layer at Mach 6: fundamental breakdown (2015, background): “As a consequence, most of the earlier experimental and numerical efforts have focused on the linear receptivity (e.g. Maslov et al. 2001; Zhong 2001) process and the linear regime of boundary layer transition (e.g. Demetriades 1960, 1977).”