Accession Number : AD0079113


Title :   ON THE HEAT TRANSFER TO THE WALLS OF A SHOCK TUBE


Corporate Author : CORNELL UNIV ITHACA NY GRADUATE SCHOOL OF AEROSPACE ENGINEERING


Personal Author(s) : ROTT, N. ; HARTUNIAN, R.


Report Date : NOV 1955


Pagination or Media Count : 47


Descriptors :   *LAMINAR BOUNDARY LAYER, *SHOCK TUBES, HEAT TRANSFER.


Distribution Statement : APPROVED FOR PUBLIC RELEASE