Print Email Facebook Twitter An analysis of shock structure and nonequilibrium laminar boundary layers induced by a normal shock wave in a ionized argon flow Title An analysis of shock structure and nonequilibrium laminar boundary layers induced by a normal shock wave in a ionized argon flow Author Liu, W.S. Institution University of Toronto Institute for Aerospace Studies Date 1975-10-30 To reference this document use: http://resolver.tudelft.nl/uuid:98c13080-82d5-4b90-a83a-b828ac944789 Publisher University of Toronto Source UTIAS Report, No. 198 Part of collection Aerospace Engineering Reports Document type report Rights (c)1975 University of Toronto Files PDF 198-2.pdf 39.15 MB Close viewer /islandora/object/uuid:98c13080-82d5-4b90-a83a-b828ac944789/datastream/OBJ/view