Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
By S. Schneider. 2004
459 citations recorded by the source corpus.
Subfields: Applied Mathematics, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/8dc1575fbc1a776cd430e13a8ebdbaa16e2acfb2
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In Applied Mathematics
In Computational Mechanics
- S. Schneider
- Hermann F. Fasel
- J. Sivasubramanian
- Xiaowen Wang
- X. Zhong
- J. Bertin
- R. Cummings
- Christoph Hader
Citations in the corpus
- Development of Hypersonic Quiet Tunnels (2008, unknown): “(1:05 10 m ) [6,7].”
- Effects of Roughness on Hypersonic Boundary-Layer Transition (2007, unknown): “methods for estimating transition on a cone frustum due to roughness on the nose tip (see [5]).”
- Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers (2012, background): “…flight data and wind tunnel experiments of the hypersonic boundary-layer transition for circular cones, scramjet forebodies, and reentry capsules (Schneider 1999, 2004, 2006); the effects of high-speed tunnel noise on transition (Schneider 2001); and experimental and flight tests of the…”
- Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels (2013, background): “However, when the nose radius or Reynolds number is increased further, transition then occurs first on the windward ray [109].”
- Critical Hypersonic Aerothermodynamic Phenomena (2006, background): “…will occur at lower altitudes, where the gas behaves as a continuum, the reader is referred to the substantial literature on the subject of rarefied gas dynamics, e.g., Schaaf (1963), Sherman (1969), Kogan (1973), Bird (1978), Yen (1984), Muntz (1989), Tirsky (1993), and Ivanov & Gimelshein (1998).”
- Direct numerical simulation of transition in a sharp cone boundary layer at Mach 6: fundamental breakdown (2015, background): “…in carrying out hypersonic boundary layer experiments (‘controlled’ experiments, in particular) and due to the existence of multiple instability modes, the role and importance of the various instability modes in a realistic transition process are not understood at all (see Schneider 2001, 2004).”