Accession Number : AD0725733
Title : Effects of Shock Wave Deceleration on Ionization Levels in a Shock Tube.
Descriptive Note : Rept. for 1 Jul 70-1 Feb 71,
Corporate Author : AEROSPACE CORP EL SEGUNDO CALIF LAB OPERATIONS
Personal Author(s) : Light,Glenn C.
Report Date : 15 JUN 1971
Pagination or Media Count : 20
Abstract : Measurements of electron density behind a decelerating shock wave in air in a shock tube are presented. A model is proposed that accounts for the effects of shock wave deceleration and boundary layer mass loss on shocked gas properties in a self-consistent manner. Calculated values of electron density based on this model are within a factor of 2 of measured values. Consequences of the combined effects of shock deceleration and boundary layer mass loss are seen to be of great importance for shock tube studies involving the determination of chemical reaction rates. (Author)
Descriptors : (*SHOCK WAVES, DECELERATION), (*PLASMA SHEATHS, ELECTRON DENSITY), SHOCK TUBES, MATHEMATICAL MODELS, BOUNDARY LAYER, GAS FLOW, CHEMICAL PROPERTIES, THERMODYNAMICS
Subject Categories : Fluid Mechanics
Plasma Physics and Magnetohydrodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE