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Shock Wave Dynamics in Weakly Ionized GasesWe have begun a comprehensive series of analyses and experiments to study the basic problem of shock wave dynamics in ionized media. Our objective is to isolate the mechanisms that are responsible for the decrease in the shock amplitude and also to determine the relevant plasma parameters that will be required for a drag reduction scheme in an actual high altitude hypersonic flight. Specifically, we have initiated a program of analyses and measurements with the objective of (i) fully characterizing the propagation dynamics in plasmas formed in gases of aerodynamic interest, (ii) isolating the mechanisms responsible for the decreased shock strength and increased shock velocity, (iii) extrapolating the laboratory observations to the technology of supersonic flight.
Document ID
19980237572
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Johnson, Joseph A., III
(Florida Agricultural and Mechanical Univ. Tallahassee, FL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Fluid Mechanics And Heat Transfer
Funding Number(s)
CONTRACT_GRANT: NAG1-1930
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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