Data & Documents

Comprehensive example data can be found in the dissertation of T. Rödiger covering the subsonic to hypersonic flow regime:

Dissertation T. Rödiger, Uni Stuttgart, 2010 (ISBN 9783868534726, DOI: https://doi.org/10.5281/zenodo.17229224):

Detection of Second Mode Instabilities

Amplitude Spectra of Second-Mode Instability under quiet flow conditions passing successive sensors on a cone at M=6
Evolution of amplified Second-Mode wave packages passing successive sensors on a flat plate at M=6

Response to a Passing Shock Wave

Signal response to passing of a shock wave in a shock tube.
Detail of the laminar region an transition to turbulent boundary layer

Rotating Detonation Engine

Surface Heat-Flux Measurements in a Rotating-Detonation Engine (presented at AIAA Scitech 2025; AIAA-2025-2146)
Detailed view of period marked in the left diagram (presented at AIAA Scitech 2025; AIAA-2025-2146)