The eN method for transition prediction: Historical review of work at TU Delft
By J. V. Ingen. 2008
261 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/2e774623c4864780c01f8ff2f892f7e256cc59d5
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Direct numerical simulations of hypersonic boundary-layer transition for a flared cone: fundamental breakdown (2019, methodology): “The N-factors are computed according to van Ingen (2008) as N = ln(A(x)/A(x0)), where A is a place holder for the amplitude and x0 is defined as the reference position where the disturbance of a given frequency and amplitude A(x0) becomes first unstable (van Ingen 2008).”