The flexible asymmetric shock tube (FAST): a Ludwieg tube facility for wave propagation measurements in high-temperature vapours of organic fluids

Journal article (2015)

Authors

T. Mathijssen Flight Performance and Propulsion - Aerospace Engineering
E.I.M. Casati Flight Performance and Propulsion - Aerospace Engineering
NR Nannan External organisation
C Zamfirescu External organisation
A Guardone External organisation
Piero Colonna Flight Performance and Propulsion - Aerospace Engineering
Research Group
Flight Performance and Propulsion (Aerospace Engineering) (TU Delft)
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Published Date

2015

Language

English

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Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Flight Performance and Propulsion