| State: | California |
|---|---|
| Address: | 1200 E California Blvd, Pasadena, CA 91125 |
| Zip code: | 91125 |
| Phone: | (626) 395-8311 |
| Website: | http://www.galcit.caltech.edu/T5/ |
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The phone number for T5 Hypervelocity Shock Tunnel is (626) 395-8311.
T5 Hypervelocity Shock Tunnel is located at 1200 E California Blvd, Pasadena, CA 91125
The website (URL) for T5 Hypervelocity Shock Tunnel is: http://www.galcit.caltech.edu/T5/
T5 Hypervelocity Shock Tunnel. H. G. Hornung^, J. E. Shepherd^ N. J. Parziale*, J. S. Jewell* California Institute of Technology ^Professors *Grad Shock wave interaction in hypervelocity flow. Air flow is left to right. Image is a holographic shadowgraph. Thesis work by S. R. Sanderson.
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T5 Hypervelocity Shock Tunnel Facility. It is a free piston shock tunnel located at California Institute of Technology, USA.It is an impulse facility capable of reaching very high stagnation temperatures and pressures at relatively high densities.
4.7 T5 Hypervelocity Shock Tunnel Facility. 5 References. Reflected shock tunnels heat and pressurize a stagnant gas by using shockwaves that are redirected back into the center; this excites the gases and produces movement, heat, and pressure.
Expansion and shock tunnels are aerodynamic testing facilities with a specific interest in high speeds and high temperature testing. Shock tunnels use steady flow nozzle expansion whereas expansion tunnels use unsteady expansion with higher enthalpy, or T5 Hypervelocity Shock Tunnel Facility.
T5 Hypervelocity Shock Tunnel Description. The main purpose of this facility is to correctly simulate hypervelocity flows by matching the enthalpy similarity Figure 3.1: Schematic diagram of the T5 Hypervelocity Shock Tunnel. The six major components are the piston, the secondary reservoir, the...
The T5 hypervelocity shock tunnel has a free-piston driver. Computations of the ow in the T5 shock tunnel show that a substantial source of noise is caused by the reection of shock waves propagating between the shock tube axis and shock tube wall in the reservoir region of the nozzle.
A nonlinear version, suitable for more generalised body shapes, is then described in the context of a series of experiments to determine the aerodynamic characteristics of the NASA Orion vehicle in the T5 hypervelocity shock tunnel.
The T5 hypervelocity shock tunnel A series of experiments has been performed in the T5 hypervelocity shock tunnel at the California Institute of Technology to determine the forces on the secondary body in several spherical proximal body configurations. however. however. for example.g...
Experiments were performed in the Hypervelocity Expansion Tube (HET) and the T5 hypervelocity shock tunnel to investigate geometric and gas composition effects on a double-wedge and double-cone geometry. The high-speed flow over the models results in a complex shock boundary-layer...