Data & Documents

Comprehensive example data can be found in the dissertation of T. Rödiger covering the subsonic to hypersonic flow regime available for download below.

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)

Dissertation T. Rödiger, Uni Stuttgart, 2010 (ISBN 9783868534726, https://doi.org/10.13140/RG.2.2.31006.45124):

Table of Contents, Dissertation, T. Rödiger, Universität Stuttgart, 2010Download
Experiments in Subsonic FlowsDownload
Experiments in Supersonic FlowsDownload
Experiments in Hypersonic FlowsDownload