Abstract — In the study of wave propagation in the free atmosphere, it is desirable to obtain time measurements to an accuracy of microsecond level. An experiment has been conducted to measure the wave speed during the propagation in the free atmosphere by the present technique. Due to sudden rupture of the diaphragm for the chamber pressure of 4.2 kg/cm2 and a wave generating in a shock tube travels with subsonic speed and the measured incident wave Mach number is 0.8 which leaves the shock tube in the free atmosphere. The measured travelling time of the incident wave to travel 61.5 cm distance in the shock tube is 2200 μsec and the same technique can apply to measure the shock wave speed. Several trigger points are installed at the exit o...
International audienceIn this work, we conduct experiments to study the interaction between a horizo...
International audienceDespite significant progresses in the understanding of the formation and propa...
The development of scramjet technology using continuos facilities is limited at present to flight Ma...
In the study of wave propagation in the free atmosphere, it is desirable to obtain time measurements...
An experimental set-up is presented for tracking the trajectory of a supersonic object using minimal...
International audienceWe conducted a series of shock tube experiments to study the influence of a cl...
This paper deals with development of velocity measurement methodology based on projectile shock wave...
This paper describes the commissioning of the flexible asymmetric shock tube (FAST), a novel Ludwieg...
International audienceThis work is about experimental study of a planar shock wave which slide over ...
An experimental study has been performed to establish investigation on the transient flows in a sup...
An experimental study has been performed to investigate transient flows in a supersonic gun tunnel. ...
Shock tube experiments are a primary means of obtaining ground test data for the hypersonic regime. ...
Experiments to ascertain the wave forms and laws of propagation and dissipation of ballistic shock w...
International audienceIn this work, we conduct experiments to study the interaction between a horizo...
International audienceDespite significant progresses in the understanding of the formation and propa...
The development of scramjet technology using continuos facilities is limited at present to flight Ma...
In the study of wave propagation in the free atmosphere, it is desirable to obtain time measurements...
An experimental set-up is presented for tracking the trajectory of a supersonic object using minimal...
International audienceWe conducted a series of shock tube experiments to study the influence of a cl...
This paper deals with development of velocity measurement methodology based on projectile shock wave...
This paper describes the commissioning of the flexible asymmetric shock tube (FAST), a novel Ludwieg...
International audienceThis work is about experimental study of a planar shock wave which slide over ...
An experimental study has been performed to establish investigation on the transient flows in a sup...
An experimental study has been performed to investigate transient flows in a supersonic gun tunnel. ...
Shock tube experiments are a primary means of obtaining ground test data for the hypersonic regime. ...
Experiments to ascertain the wave forms and laws of propagation and dissipation of ballistic shock w...
International audienceIn this work, we conduct experiments to study the interaction between a horizo...
International audienceDespite significant progresses in the understanding of the formation and propa...
The development of scramjet technology using continuos facilities is limited at present to flight Ma...