Restricted Shock Separation in Rocket Nozzles
By M. Frey, G. Hagemann. 2000
174 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/ea23e5458f9760e5f373361176c7f97e47672e1a
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In Aerospace Engineering
In Applied Mathematics
In Computational Mechanics
Citations in the corpus
- A scaling analysis for turbulent shock-wave/boundary-layer interactions (2013, background): “…& Babinsky 2008; Bur et al. 2008), blunt fin interactions (Brusniak & Dolling 1994; Ünalmis & Dolling 1996; Bueno 2006), over-expanded nozzles (Frey & Hagemann 1998, 2000; Bourgoing & Reijasse 2005), compression ramp interactions (Thomke & Roshko 1969; Spaid & † Email address for…”