Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

By J. Wagner, K. Yuceil, A. Valdivia, N. Clemens, D. Dolling. 2009

333 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/32715952f73c4ecb5618391c6333efe2ba4fbe64

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1. J. Martinez Schramm
2. K. Hannemann
3. S. Laurence
4. S. Karl

Citations in the corpus

• Transient fluid-combustion phenomena in a model scramjet (2013, methodology): “The oscillations from roughly 8 ms are similar to those documented, for example, by Tan & Guo (2007) and Wagner et al. (2009) for an unstarted inlet (this oscillatory behaviour is often referred to as “buzzing” and is caused by periodic gorging and disgorging of the inlet shock system).”