Accession Number : AD0158942

Title :   ATTENUATION IN A SHOCK TUBE DUE TO UNSTEADY-BOUNDARY-LAYER ACTION

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C

Personal Author(s) : Mireis,Harold

Report Date : 24 APR 1956

Pagination or Media Count : 1

Descriptors :   *ATTENUATION, *SHOCK WAVES, BOUNDARY LAYER, MATHEMATICAL ANALYSIS, PRESSURE

Distribution Statement : APPROVED FOR PUBLIC RELEASE