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Accession Number:
AD0158942
Title:
ATTENUATION IN A SHOCK TUBE DUE TO UNSTEADY-BOUNDARY-LAYER ACTION
Descriptive Note:
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C
Report Date:
1956-04-24
Pagination or Media Count:
1.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE
