Abstract
An experimental,research program designed to evaluate the effect of a weakly ionized gas on a propagating shock wave is described. This research was performed in a “large” diameter (4”) shock tube at “near” room temperature (314 K) in 20 Torr Helium, usjng an acoustic pressure se&or to measure the intensity of the shock wave. The initial results from this program indicate that the intensity of the shock is reduced by 25-50% when the Helium is weakly ionized, with ionization fractions on the order of 10-8, while no significant changes in the shock propagation speed are observed.
Original language | English |
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Pages | 1-8 |
Number of pages | 8 |
DOIs | |
State | Published - 1999 |
Event | 9th International Space Planes and Hypersonic Systems and Technologies Conference, 1999 - Norfolk, United States Duration: Nov 1 1999 → Nov 4 1999 |
Conference
Conference | 9th International Space Planes and Hypersonic Systems and Technologies Conference, 1999 |
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Country/Territory | United States |
City | Norfolk |
Period | 11/1/99 → 11/4/99 |