On the formation of Friedlander waves in a compressed-gas-driven shock tube.
Compressed-gas-driven shock tubes have become popular as a laboratory-scale replacement for field blast tests. The well-known initial structure of the Riemann problem eventually evolves into a shock structure thought to resemble a Friedlander wave, although this remains to be demonstrated theoretically. In this paper, we develop a semi-analytical model to predict the key characteristics of pseudo blast waves forming in a shock tube: location where the wave first forms, peak over-pressure, decay time and impulse. The approach is based on combining the solutions of the two different types of wave interactions that arise in the shock tube after the family of rarefaction waves in the Riemann solution interacts with the closed end of the tube. The results of the analytical model are verified against numerical simulations obtained with a finite volume method. The model furnishes a rational approach to relate shock tube parameters to desired blast wave characteristics, and thus constitutes a useful tool for the design of shock tubes for blast testing.
Institute for Solider Nanotechnologies , Department of Aeronautics and Astronautics, Massachusetts Institute of Technology , Cambridge, MA 02139, USA.
Abiy F
AF
Tasissa
Institute for Solider Nanotechnologies , Department of Aeronautics and Astronautics, Massachusetts Institute of Technology , Cambridge, MA 02139, USA.
Martin
M
Hautefeuille
US Army Natick Soldier Research , Development and Engineering Center , Natick, MA 01760, USA.
John H
JH
Fitek
Institute for Solider Nanotechnologies , Department of Aeronautics and Astronautics, Massachusetts Institute of Technology , Cambridge, MA 02139, USA.
Raúl A
RA
Radovitzky
Friedlander waves; blast waves; shock tubes